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Broadway Tower was the brainchild of the great 18th century landscape gardener, Capability Brown. His vision was carried out for George William, 6th Earl of Coventry with the help of renowned architect James Wyatt and completed in 1798.
The location for the Tower was wisely chosen: a dramatic outlook on a pre-medieval trading route and beacon hill.
Wyatt designed his "Saxon Tower" as an eccentric amalgamation of architectural components ranging from turrets, battlements and gargoyles to balconies.
The Tower stands 65 feet (20 metres) high.
Beautiful fallow deer photographed in Petworth Park during the rutting season.
The fallow deer (Dama dama) is a ruminant mammal belonging to the family Cervidae. This common species is native to western Eurasia, but has been introduced widely elsewhere. It often includes the rarer Persian fallow deer as a subspecies (D. d. mesopotamica), while others treat it as an entirely different species (D. mesopotamica).
Petworth House and Park in Petworth, West Sussex, England, has been a family home for over 800 years. The estate was a royal gift from the widow of Henry I to her brother Jocelin de Louvain, who soon after married into the renowned Percy family. As the Percy stronghold was in the north, Petworth was originally only intended for occasional use.
Petworth, formerly known as Leconfield, is a major country estate on the outskirts of Petworth, itself a town created to serve the house. Described by English Heritage as "the most important residence in the County of Sussex", there was a manorial house here from 1309, but the present buildings were built for the Dukes of Somerset from the late 17th century, the park being landscaped by "Capability" Brown. The house contains a fine collection of paintings and sculptures.
The house itself is grade I listed (List Entry Number 1225989) and the park as a historic park (1000162). Several individual features in the park are also listed.
It was in the late 1500s that Petworth became a permanent home to the Percys after Elizabeth I grew suspicious of their allegiance to Mary, Queen of Scots and confined the family to the south.
The 2nd Earl of Egremont commissioned Capability Brown to design and landscape the deer park. The park, one of Brownâs first commissions as an independent designer, consists of 700 acres of grassland and trees. It is inhabited by the largest herd of fallow deer in England. There is also a 12-hectare (30-acre) woodland garden, known as the Pleasure Ground.
Brown removed the formal garden and fishponds of the 1690âs and relocated 64,000 tons of soil, creating a serpentine lake. He bordered the lake with poplars, birches and willows to make the ânaturalâ view pleasing. A 1987 hurricane devastated the park, and 35,000 trees were planted to replace the losses. Gracing the 30 acres of gardens and pleasure grounds around the home are seasonal shrubs and bulbs that include lilies, primroses, and azaleas. A Doric temple and Ionic rotunda add interest in the grounds.
Petworth House is a late 17th-century mansion, rebuilt in 1688 by Charles Seymour, 6th Duke of Somerset, and altered in the 1870s by Anthony Salvin. The site was previously occupied by a fortified manor house founded by Henry de Percy, the 13th-century chapel and undercroft of which still survive.
Today's building houses an important collection of paintings and sculptures, including 19 oil paintings by J. M. W. Turner (some owned by the family, some by Tate Britain), who was a regular visitor to Petworth, paintings by Van Dyck, carvings by Grinling Gibbons and Ben Harms, classical and neoclassical sculptures (including ones by John Flaxman and John Edward Carew), and wall and ceiling paintings by Louis Laguerre. There is also a terrestrial globe by Emery Molyneux, believed to be the only one in the world in its original 1592 state.
For the past 250 years the house and the estate have been in the hands of the Wyndham family â currently Lord Egremont. He and his family live in the south wing, allowing much of the remainder to be open to the public.
The house and deer park were handed over to the nation in 1947 and are now managed by the National Trust under the name "Petworth House & Park". The Leconfield Estates continue to own much of Petworth and the surrounding area. As an insight into the lives of past estate workers the Petworth Cottage Museum has been established in High Street, Petworth, furnished as it would have been in about 1910.
Croome, Worcestershire. The Drawing Room was remodelled with a heightened ceiling, which caused the loss of two bedrooms above. Both house and gardens at Croome Court were designed by Capability Brown between 1751-2, rebuilding an earlier house from the 1640s. The estate was requisitioned in WW2, but was not used for troops, being offered to the Dutch Royal family, but nearby, and partly within the grounds, RAF Defford was established, an important location for the Telecommunications Research Establishment. They left in 1957 as the runways were too short. The house was sold by the Croome Estate Trust in 1948, and became St Josephs Special School until 1979. Taken over by the Hare Krishna movement, it became known as Chaitanya College with involvement from George Harrison, who created recording studios within the house. They left in 1984 and the house was used for several short-term activities, including a training centre; apartments; a restaurant and conference centre; a hotel and golf course, and a private family home. In 2007, it was purchased by the Croome Heritage Trust, who leased it to the National Trust. Croome Court is grade 1 listed.
Croome D'Abitot, near Pershore, Worcestershire, West Midlands, England - Croome Court, High Green
June 2025
"Prior Park Landscape Garden is an 18th-century landscape garden, designed by the poet Alexander Pope and the landscape gardener Capability Brown, and now owned by the National Trust. It is south of Bath, Somerset, England by Ralph Allen Drive, and 3/4 mile (1.2 km) from the Kennet and Avon canal path. The garden was influential in defining the style of garden known as the "English garden" in continental Europe.... The 28 acre (113,000 m²) landscape garden is set in a dramatic site running down a small steep valley, with fine views of the city of Bath. Its many interesting features include a Palladian bridge (one of only 4 left in the world), Gothic temple, gravel cabinet, Mrs Allen's Grotto, and three lakes plus a serpentine lake. The Palladian bridge has been designated as a Grade I listed building and Scheduled Ancient Monument." --Wikipedia
A lovely, if chilly, autumnal Sunday afternoon in the park of gardens of Blenheim Palace. This is the view north-west from the palace, overlooking part of the lake that was formed when renowned landscape gardner, Capability Brown dammed the River Glyme. Past the trees is the Column of Victory - 41m tall and topped with a classical statue of the 1st Duke of Malborough. Today the Palace and gardens are designated a world heritage site and enjoyed by a large number of visitors
NASA’s Space Launch System (SLS) rocket with the Orion spacecraft atop a mobile launcher is seen through the windows of Firing Room 1 in the Rocco A. Petrone Launch Control Center as it rolls out of High Bay 3 of the Vehicle Assembly Building to Launch Complex 39B, on Tuesday, Aug. 16, 2022, ahead of the agency’s Artemis I flight test. The fully stacked and integrated SLS rocket and Orion spacecraft is scheduled to liftoff on Monday, Aug. 29. The first in a series of increasingly complex missions, Artemis I will provide a foundation for human deep space exploration and demonstrate our commitment and capability to extend human presence to the Moon and beyond. The primary goal of Artemis I is to thoroughly test the integrated systems before crewed missions by launching Orion atop the SLS rocket, operating the spacecraft in a deep space environment, testing Orion’s heat shield, and recovering the crew module after reentry, descent, and splashdown. In later missions, NASA will land the first woman and the first person of color on the surface of the Moon, paving the way for a long-term lunar presence and serving as a steppingstone on the way to Mars. Photo credit: NASA/Isaac Watson
+++ DISCLAIMER +++Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!
Some background:
The Gudkov Gu-1 was a Soviet fighter aircraft produced shortly after World War II in small numbers at the start of the jet age, but work on the Gudkov Gu-1 already started in 1944. Towards the end of World War II the Soviet Union saw the need for a strategic bombing capability similar to that of the United States Army Air Forces. The Soviet VVS air arm had the locally designed Petlyakov Pe-8 four-engined heavy bomber in service at the start of the war, but only 93 had been built by the end of the war and the type had become obsolete. By that time the U.S. regularly conducted bombing raids on Japan from distant Pacific forward bases using B-29 Superfortresses, and the Soviet Air Force lacked this capability.
Joseph Stalin ordered the development of a comparable bomber, and the U.S. twice refused to supply the Soviet Union with B-29s under Lend Lease. However, on four occasions during 1944, individual B-29s made emergency landings in Soviet territory and one crashed after the crew bailed out. In accordance with the Soviet–Japanese Neutrality Pact, the Soviets were neutral in the Pacific War and the bombers were therefore interned and kept by the Soviets. Despite Soviet neutrality, America demanded the return of the bombers, but the Soviets refused. Three repairable B-29s were flown to Moscow and delivered to the Tupolev OKB. One B-29 was dismantled, the second was used for flight tests and training, and the third one was left as a standard for cross-reference.
Stalin told Tupolev to clone the Superfortress in as short a time as possible. The reverse-engineering effort involved 900 factories and research institutes, who finished the design work during the first year. 105,000 drawings were made, and the American technology had to be adapted to local material and manufacturing standards – and ended in a thorough re-design of the B-29 “under the hood”. By the end of the second year, the Soviet industry was to produce 20 copies of the aircraft ready for State acceptance trials.
While work on what would become the Tupolev Tu-4 was on the way, the need for a long range escort fighter arose, too. Soviet officials were keen on the P-51 Mustang, but, again, the USA denied deliveries, so that an indigenous solution had to be developed. With the rising tension of international relationships, this became eventually the preferred solution, too.
While the design bureau Lavochkin had already started with work on the La-9 fighter (which entered service after WWII) and the jet age was about to begin, the task of designing a long range escort fighter for the Tu-4 was relegated to Mikhail I. Gudkov who had been designing early WWII fighters like the LaGG-1 and -3 together with Lavochkin. Internally, the new fighter received the project handle "DIS" (Dalnij Istrebitel' Soprovozhdenya ="long-range escort fighter").
In order to offer an appropriate range and performance that could engage enemy interceptors in the bombers’ target area it was soon clear that neither a pure jet nor a pure piston-engine fighter was a viable solution – a dilemma the USAAF was trying to solve towards 1945, too. The jet engine alone did not offer sufficient power, and fuel consumption was high, so that the necessary range could never be achieved with an agile fighter. Late war radials had sufficient power and offered good range, but the Soviet designers were certain that the piston engine fighter had no future – especially when fast jet fighters had to be expected over enemy territory.
Another problem arose through the fact that the Soviet Union did not have an indigenous jet engine at hand at all in late 1945. War booty from Germany in the form of Junkers Jumo 004 axial jet engines and blueprints of the more powerful HeS 011 were still under evaluation, and these powerplants alone did neither promise enough range nor power for a long range fighter aircraft. Even for short range fighters their performance was rather limited – even though fighters like the Yak-15 and the MiG-9 were designed around them.
After many layout experiments and calculation, Gudkov eventually came up with a mixed powerplant solution for the DIS project. But unlike the contemporary, relatively light I-250 (also known as MiG-13) interceptor, which added a mechanical compressor with a primitive afterburner (called VRDK) to a Klimov VK-107R inline piston engine, the DIS fighter was equipped with a powerful radial engine and carried a jet booster – similar to the US Navy’s Ryan FR-1 “Fireball”. Unlike the FR-1, though, the DIS kept a conservative tail-sitter layout and was a much bigger aircraft.
The choice for the main powerplant fell on the Shvetsov ASh-82TKF engine, driving a large four blade propeller. This was a boosted version of the same 18 cylinder twin row radial that powered the Tu-4, the ASh-73. The ASh-82TKF for the escort fighter project had a rating of 2,720 hp (2,030 kW) while the Tu-4's ASh-73TK had "only" a temporary 2,400 hp (1,800 kW) output during take-off. The airframe was designed around this massive and powerful engine, and the aircraft’s sheer size was also a result of the large fuel capacity which was necessary to meet the range target of at least 3.000 km (1.860 mi, 1.612 nmi).
The ASh-82TKF alone offered enough power for a decent performance, but in order to take on enemy jet fighters and lighter, more agile propeller-driven fighters, a single RD-20 axial-flow turbojet with 7.8 kN (1,754 lbf) thrust was added in the rear-fuselage. It was to add power for take-off and in combat situations only. Its fixed air intakes were placed on the fuselage flanks, right behind the cockpit, and the jet pipe was placed under the fin and the stabilizers.
Outwardly, Gudkov’s DIS resembled the late American P-47D or the A-1 Skyraider a lot, and the beefy aircraft was comparable in size and weight, too. But the Soviet all-metal aircraft was a completely new construction and featured relatively small and slender laminar flow wings. The wide-track landing gear retracted inwards into the inner wings while the tail wheel retracted fully into a shallow compartment under the jet pipe.
The pilot sat in a spacious cockpit under a frameless bubble canopy with very good all-round visibility and enjoyed amenities for long flights such as increased padding in the seat, armrests, and even a urinal. In addition, a full radio navigation suite was installed for the expected long range duties over long stretches of featureless landscape like the open sea.
Armament consisted of four 23 mm Nudelman-Suranov NS-23 cannons with 100 RPG in the wings, outside of the propeller arc. The guns were good for a weight of fire of 6kg (13.2 lb)/sec, a very good value. Five wet hardpoints under the fuselage, the wings outside of the landing gear well and under the wing tips could primarily carry auxiliary drop tanks or an external ordnance of up to 1.500 kg (3.300 lb).
Alternatively, iron bombs of up to 500 kg (1.100 lb) caliber could be carried on the centerline pylon, and a pair of 250 kg (550 lb) bombs under the wings, but a fighter bomber role was never seriously considered for the highly specialized and complex aircraft.
The first DIS prototype, still without the jet booster, flew in May 1947. The second prototype, with both engines installed, had its fuel capacity increased by an additional 275 l (73 US gal) in an additional fuel tank behind the cockpit. The aircraft was also fitted with larger tires to accommodate the increased all-up weight, esp. with all five 300 l drop tanks fitted for maximum range and endurance.
Flight testing continued until 1948 and the DIS concept proved to be satisfactory, even though the complicated ASh-82TKF hampered the DIS’ reliability - to the point that fitting the ASh-73TK from the Tu-4 was considered for serial production, even if this would have meant a significant reduction in performance. The RD-20 caused lots of trouble, too. Engine reliability was generally poor, and re-starting the engine in flight did not work satisfactorily – a problem that, despite several changes to the starter and ignition system, could never be fully cured. The jet engine’s placement in the tail, together with the small tail wheel, also caused problems because the pilots had to take care that the tail would not aggressively hit the ground upon landings, because the RD-20 and its attachments were easily damaged.
Nevertheless, the DIS basically fulfilled the requested performance specifications and was, despite many shortcomings, eventually cleared for production in mid 1948. It received the official designation Gudkov Gu-1, honoring the engineer behind the aircraft, even though the aircraft was produced by Lavochkin.
The first machines were delivered to VVS units in early 1949 - just in time for the Tu-4's service introduction after the Russians had toiled endlessly on solving several technical problems. In the meantime, jet fighter development had quickly progressed, even though a purely jet-powered escort fighter for the Tu-4 was still out of question. Since the Gu-1 was capricious, complex and expensive to produce, only a limited number left the factories and emphasis was put on the much simpler and more economical Lavochkin La-11 escort fighter, a lightweight evolution of the proven La-9. Both types were regarded as an interim solution until a pure jet escort fighter would be ready for service.
Operationally the Gu-1s remained closely allocated to the VVS’ bomber squadrons and became an integral part of them. Anyway, since the Tu-4 bomber never faced a serious combat situation, so did the Gu-1, which was to guard it on its missions. For instance, both types were not directly involved in the Korean War, and the Gu-1 was primarily concentrated at the NATO borders to Western Europe, since bomber attacks in this theatre would certainly need the heavy fighter’s protection.
The advent of the MiG-15 - especially the improved MiG-15bis with additional fuel capacities and drop tanks, quickly sounded the death knell for the Gu-1 and any other post-WWII piston-engine fighter in Soviet Service. As Tu-4 production ended in the Soviet Union in 1952, so did the Gu-1’s production after only about 150 aircraft. The Tu-4s and their escort fighters were withdrawn in the 1960s, being replaced by more advanced aircraft including the Tupolev Tu-16 jet bomber (starting in 1954) and the Tupolev Tu-95 turboprop bomber (starting in 1956).
The Gudkov Gu-1, receiving the NATO ASCC code “Flout”, remained a pure fighter. Even though it was not a success, some proposals for updates were made - but never carried out. These included pods with unguided S-5 air-to-air-rockets, to be carried on the wing hardpoints, bigger, non-droppable wing tip tanks for even more range or, alternatively, the addition of two pulsejet boosters on the wing tips.
There even was a highly modified mixed powerplant version on the drawing boards in 1952, the Gu-1M. Its standard radial powerplant for cruise flight was enhanced with a new, non-afterburning Mikulin AM-5 axial flow jet engine with 2.270 kgf/5,000 lbf/23 kN additional thrust in the rear fuselage. With this temporary booster, a top speed of up to 850 km/h was expected. But to no avail - the pure jet fighter promised a far better performance and effectiveness, and the Gu-1 remained the only aircraft to exclusively carry the Gudkov name.
General characteristics:
Crew: 1
Length: 12 m (39 ft 4 in)
Wingspan: 14 m (45 ft 11 in)
Height: 4.65 m (15 ft 3 in)
Wing area: 28 m² (301.388 ft²)
Airfoil:
Empty weight: 4,637 kg (10,337 lb)
Loaded weight: 6.450 kg (14.220 lb)
Maximum take-off weight: 7,938 kg (17,500 lb)
Powerplant:
1× Shvetsov ASh-82TKF 18-cylinder air-cooled radial engine, rated at 2,720 hp (2,030 kW)
1x RD-20 axial-flow turbojet with 7.8 kN (1,754 lbf) thrust as temporary booster
Performance
Maximum speed: 676 km/h (420 mph) at 29,000 ft (8,839 m) with the radial only,
800 km/h (497 mph/432 kn,) with additional jet booster
Cruise speed: 440 km/h (237 kn, 273 mph)
Combat radius: 820 nmi (945 mi, 1,520 km)
Maximum range: 3.000 km (1.860 mi, 1.612 nmi) with drop tanks
Service ceiling: 14,680 m (48,170 ft)
Wing loading: 230.4 kg/m² (47.2 lb/ft²)
Power/mass: 0.28 kW/kg (0.17 hp/lb)
Climb to 5,000 m (16,400 ft): 5 min 9 sec;
Climb to 10,000 m (32,800 ft): 17 min 38 sec;
Climb to 13,000 m (42,640 ft): 21 min 03 sec
Armament
4× 23 mm Nudelman-Suranov NS-23 cannons with 100 RPG in the outer wings
Five hardpoints for an external ordnance of 1.500 kg (3.300 lb)
The kit and its assembly:
This whif is the incarnation of a very effective kitbashing combo that already spawned my fictional Japanese Ki-104 fighter, and it is another submission to the 2018 “Cold War” group build at whatifmodelers.com. This purely fictional Soviet escort fighter makes use of my experiences from the first build of this kind, yet with some differences.
The kit is a bashing of various parts and pieces:
· Fuselage, wing roots, landing gear and propeller from an Academy P-47D
· Wings from an Ark Model Supermarine Attacker (ex Novo)
· Tail fin comes from a Heller F-84G
· The stabilizers were taken from an Airfix Ki-46
· Cowling from a Matchbox F6F, mounted and blended onto the P-47 front
· Jet exhaust is the intake of a Matchbox Me 262 engine pod
My choice fell onto the Academy Thunderbolt because it has engraved panel lines, offers the bubble canopy as well as good fit, detail and solid material. The belly duct had simply been sliced off, and the opening later faired over with styrene sheet and putty, so that the P-47’s deep belly would not disappear.
The F6F cowling was chosen because it looks a lot like the ASh-73TK from the Tu-4. But this came at a price: the P-47 cowling is higher, tighter and has a totally different shape. It took serious body sculpting with putty to blend the parts into each other. Inside of the engine, a styrene tube was added for a metal axis that holds the uncuffed OOB P-47 four blade propeller. The P-47’s OOB cockpit tub was retained, too, just the seat received scratched armrests for a more luxurious look.
The Attacker wings were chosen because of their "modern" laminar profile. The Novo kit itself is horrible and primitive, but acceptable for donations. OOB, the Attacker wings had too little span for the big P-47, so I decided to mount the Thunderbolt's OOB wings and cut them at a suitable point: maybe 0.5", just outside of the large main wheel wells. The intersection with the Attacker wings is almost perfect in depth and width, relatively little putty work was necessary in order to blend the parts into each other. I just had to cut out new landing gear wells from the lower halves of the Attacker wings, and with new attachment points the P-47’s complete OOB landing gear could be used.
With the new wing shape, the tail surfaces had to be changed accordingly. The trapezoid stabilizers come from an Airfix Mitsubishi Ki-46, and their shape is a good match. The P-47 fin had to go, since I wanted something bigger and a different silhouette. The fuselage below was modified with a jet exhaust, too. I actually found a leftover F-84G (Heller) tail, complete with the jet pipe and the benefit that it has plausible attachment points for the stabilizers far above the jet engine in the Gu-1’s tail.
However, the F-84 jet pipe’s diameter turned out to be too large, so I went for a smaller but practical alternative, a Junkers Jumo 004 nacelle from a Me 262 (the ancestor of the Soviet RD-20!). Its intake section was cut off, flipped upside down, the fin was glued on top of it and then the new tail was glued to the P-47 fuselage. Some (more serious) body sculpting was necessary to create a more or less harmonious transition between the parts, but it worked.
The plausible placement of the air intakes and their shape was a bit of a challenge. I wanted them to be obvious, but still keep an aerodynamic look. An initial idea had been to keep the P-47’s deep belly and widen the central oil cooler intake under the nose, but I found the idea wacky and a bit pointless, since such a long air duct would not make much sense since it would waste internal space and the long duct’s additional weight would not offer any benefit?
Another idea were air intakes in the wing roots, but these were also turned down since the landing gear wells would be in the way, and placing the ducts above or below the wings would also make no sense. A single ventral scoop (looking like a P-51 radiator bath) or two smaller, dorsal intakes (XP-81 style) behind the cockpit were other serious candidates – but these were both rejected because I wanted to keep a clean side profile.
I eventually settled for very simple, fixed side intakes, level with the jet exhaust, somewhat inspired by the Lavochkin La-200B heavy fighter prototype. The air scoops are simply parts from an Italeri Saab 39 Gripen centerline drop tank (which has a flat, oval diameter), and their shape is IMHO a perfect match.
Painting and markings:
While the model itself is a wild mix of parts with lots of improvisation involved, I wanted to keep the livery rather simple. The most plausible choice would have been an NMF finish, but I rather wanted some paint – so I used Soviet La-9 and -11 as a benchmark and settled for a simple two-tone livery: uniform light grey upper and light blue lower surfaces.
I used RAF Medium Sea Grey (Humbrol 165) and Soviet Underside Blue (Humbrol 114) as basic tones, and, after a black ink wash, these were lightened up through dry-brushed post-shading. The yellow spinner and fin tip are based on typical (subtle) squadron markings of the late 40ies era.
The cockpit as well the engine and landing gear interior became blue-grey (Revell 57), similar to the typical La-9/11’s colors. The green wheel discs and the deep blue propeller blades are not 100% in the aircraft's time frame, but I added these details in order to enhance the Soviet touch and some color accents.
Tactical markings were kept simple, too. The "38" and the Red Stars come form a Mastercraft MiG-15, the Guards badge from a Begemoth MiG-25 sheet and most of the stencils were taken from a Yak-38 sheet, also from Begemoth.
Finally, the kit was sealed with matt acrylic varnish (Italeri) and it received some mild soot stains and chipped paint around the cockpit and on the leading edges. Some oil stains were added around the engine (with Tamiya Smoke), too.
A massive aircraft, and this new use of the P-47/Attacker combo results again in a plausible solution. The added jet engine might appear a bit exotic, but the mixed powerplant concept was en vogue after WWII, but only a few aircraft made it beyond the prototype stage.
While painting the model I also wondered if an all dark blue livery and some USN markings could also have made this creation the Grumman JetCat? With the tall fin, the Gu-1 could also be an F8F Bearcat on steroids? Hmmm...
Harcourt Arboretum
The University of Oxford Arboretum
Acquired by the University in 1947 from the Harcourt family. It is now an integral part of the tree and plant collection of the University of Oxford Botanic Garden.
The original Pinetum, which forms the core of the arboretum, was laid out by William Sawrey Gilpin in the 1830s. Gilpin was a leading promoter of the picturesque style of planting and advised the Harcourt family on the establishment and layout of the arboretum. The trees are now mature, with Giant Redwoods and Monkey-Puzzle trees in the collection.
The arboretum also contains some of the finest conifer collections in the UK all set within 130 acres of historic Capability Brown landscape. The grounds include a 10-acre typical English woodland and a 37-acre summer flowering meadow.
The creation of the Blenheim lake by Capability Brown flooded a dry valley and this wonderful prospect was the result. It's one of my favourite parts of the Blenheim park, it's quiet and a haven for birdlife. I have photographed this scene in all the seasons and it always looks good!
Ickworth House, Horringer, Bury St Edmunds, Suffolk
The House was built between the years of 1795 and 1829 to the designs of the Italian Architect Mario Asprucci, his most noted work being the Villa Borghese. It was this work that Frederick Hervey, the then 4th Earl of Bristol and Bishop of Derry had seen.
Asprucci’s plans were then taken up by the brothers Francis & Joseph Sandys, English architects.
The Parkland, of which there is 1,800 acres in total, was designed by Capability Brown and was Italianate in style. This style much loved by the 4th Earl.
Most of the friezes running around the rotunda were based upon John Flaxman’s illustrations of The Iliad and The Odyssey although, within the entrance portico there are some panels designed by Lady Caroline, the Earl’s Granddaughter and are based upon the Roman Olympic Games.
There are many works of art inside the house and very much well worth the visit.
At the week-end of Her Majesty the Queen’s 90th Birthday, HMS Kent arrives at London for formal events. Picture: POA(Phot) Owen Cooban
HMS Kent visits London today and will be in this weekend during the year of Her Majesty the Queen’s 90th Birthday. The Ship will conduct a Capability Demonstration on 13 May for guests, including representatives of London’s emergency services, showing how a typical Royal Navy Frigate operates on a daily basis. The demonstration will show the Royal Navy’s ability to deliver defence diplomacy and disaster relief, through to high end warfighting. The Ship will also host a series of formal events to which affiliates and local dignitaries have been invited.
DDC-16-149
Croome Court is a mid 18th century Neo-Palladian mansion surrounded by an extensive landscaped parkland at Croome D'Abitot, near Pershore in south Worcestershire. The mansion and park were designed by Lancelot "Capability" Brown for George Coventry, 6th Earl of Coventry, and was Brown's first landscape design and first major architectural project. Some of the internal rooms of the mansion were designed by Robert Adam.
The mansion house is owned by Croome Heritage Trust, and is leased to the National Trust who operate it, along with the surrounding parkland, as a tourist attraction. The National Trust own the surrounding parkland, which is also open to the public.
Location[edit]
Croome Court is located near to Croome D'Abitot, in Worcestershire,[1] near Pirton, Worcestershire.[2] The wider estate was established on lands that were once part of the royal forest of Horewell.[3] Traces of these older landscapes, such as unimproved commons and ancient woodlands, can be found across the former Croome Estate.[4]
House[edit]
Croome Court South Portico
History[edit]
The foundations and core of Croome Court, including the central chimney stack structure, date back to the early 1640s.[5] Substantial changes to this early house were made by Gilbert Coventry, 4th Earl of Coventry.[6]
In 1751, George Coventry, the 6th Earl, inherited the estate, along with the existing Jacobean house. He commissioned Lancelot "Capability" Brown, with the assistance of Sanderson Miller, to redesign the house and estate.[7][1] It was Brown's "first flight into the realms of architecture" and a "rare example of his architectural work",[8] and it is an important and seminal work.[9] It was built between 1751 and 1752, and it and Hagley Hall are considered to be the finest examples of Neo-Palladian architecture in Worcestershire. Notable Neo-Palladian features incorporated into Croome Court include the plain exterior and the corner towers with pyramidal roofs (a feature first used by Inigo Jones in the design of Wilton House in Wiltshire).[1] Robert Adam worked on the interior of the building from 1760 onwards.[10]
The house has been visited by George III,[2][11] as well as Queen Victoria[7] during summers when she was a child, and George V (then Duke of York).[11]
A jam factory was built by the 9th Earl of Coventry, near to Pershore railway station, in about 1880, to provide a market for Vale of Evesham fruit growers in times of surplus. Although the Croome connection with jam making had ceased, during the First World War, the building was leased by the Croome Estate Trust to the Huddersfield Fruit Preserving Company as a pulping station.[12]
The First World War deeply affected Croome, with many local casualties, although the house was not requisitioned for the war effort. This is possibly because it was the home of the Lord Lieutenant of the County, who needed a residence for his many official engagements.[13]
During the Second World War Croome Court was requisitioned by the Ministry of Works and leased for a year to the Dutch Government as a possible refuge for Queen Wilhelmina of the Netherlands; to escape the Nazi occupation of the Netherlands. However, evidence shows that they stayed two weeks at the most, perhaps because of the noise and fear created by the proximity of Defford Aerodrome. They later emigrated to Canada.[14]
In 1948 the Croome Estate Trust sold the Court, along with 38 acres (15 ha) of land, to the Roman Catholic Archdiocese of Birmingham, and the mansion became St Joseph's Special School, which was run by nuns[15] from 1950[11] until 1979.[15]
The house was listed on 11 August 1952; it is currently Grade I listed.[10]
In 1979 the hall was taken over by the International Society for Krishna Consciousness (Hare Krishna movement), who used it as their UK headquarters and a training college[16] called Chaitanya College,[15] run by 25 members of the movement.[16] During their tenure they repainted the Dining Room.[17] In 1984 they had to leave the estate for financial reasons. They held a festival at the hall in 2011.[16]
From 1984 onwards various owners tried to use the property as a training centre; apartments; a restaurant and conference centre; and a hotel and golf course,[15] before once more becoming a private family home,[2][15] with outbuildings converted to private houses.[15]
The house was purchased by the Croome Heritage Trust, a registered charity,[18] in October 2007,[19] and it is now managed by the National Trust as a tourist attraction. It opened to the public in September 2009, at which point six of the rooms had restored, costing £400,000, including the Saloon. It was estimated that another £4 million[2][20] to £4.8 million would be needed to restore the entire building. Fundraising activities for the restoration included a 2011 raffle for a Morgan sports car organised by Lord and Lady Flight. After the restoration is complete, a 999-year lease on the building will be granted to the National Trust.[21] An oral history project to record recollections about Croome was funded by the Heritage Lottery Fund.[15] As of 2009, the service wing was empty and in need of substantial repair.[22]
Exterior[edit]
The mansion is faced with Bath stone,[7] limestone ashlar, and has both north and south facing fronts. It has a basement and two stories, with three stories in the end pavilions. A slate roof, with pyramid roofs over the corner towers, tops the building, along with three pair-linked chimneys along the axis of the house.[10]
Both fronts have 11 bays, split into three central sets of three each, and one additional bay each side. The north face has a pedimented centre, with two balustraded staircases leading to a Roman Doric doorcase. The south face has a projecting Ionic tetrastyle portico and Venetian windows. It has a broad staircase, with cast stone sphinxes on each side, leading to a south door topped with a cornice on consoles. The wings have modillion cornice and balustrade.[10]
A two-story L-shaped service wing is attached to the east side of the mansion. It is made of red brick and stone, with slate roofs.[10] It was designed by Capability Brown in 1751-2.[22] On the far side of the service wing, a wall connects it to a stable court.[10]
Interior[edit]
The interior of the house was designed partially by Capability Brown, with plasterwork by G. Vassalli, and partially by Robert Adam, with plasterwork by J. Rose Jr. It has a central spine corridor. A stone staircase, with iron balusters, is at the east end.[10]
The entrance hall is on the north side of the building, and has four fluted Doric columns, along with moulded doorcases. To the east of the entrance hall is the dining room, which has a plaster ceiling and cornice, while to the west is a billiard room, featuring fielded panelling, a plaster cornice, and a rococo fireplace. The three rooms were probably decorated around 1758-59 by Capability Brown.[10] The dining room was vibrantly repainted by the Hare Krishnas in the 1970s-80s.[17]
The central room on the south side is a saloon, probably by Brown and Vassalli. It has an elaborate ceiling, with three panels, deep coving, and a cornice, along with two Ionic fireplaces, and Palladian doorcases.[10] George III was entertained by George Coventry, the 6th Earl, in the house's Saloon.[2] A drawing room is to the west of the saloon, and features rococo plasterwork and a marble fireplace.[10]
To the east of the saloon is the Tapestry Room.[10] This was designed in 1763-71, based on a design by Robert Adam, and contained tapestries and furniture covers possibly designed by Jacques Germain Soufflot, and made by Manufacture Nationale des Gobelins.[23] Around 1902 the ninth Earl sold the tapestries and seating to a Parisian dealer. In 1949 the Samuel H. Kress Foundation purchased the ceiling, floor, mantlepiece, chair rails, doors and the door surrounds, which were donated to the Metropolitan Museum of Art, New York, in 1958. In 1959 the Kress Foundation also helped the Metropolitan Museum acquire the chair and sofa frames, which they recovered using the original tapestry seats.[7][23] A copy of the ceiling was installed in place of the original.[10] As of 2016, the room is displayed as it would have looked after the tapestries had been sold, with a jug and ewer on display as the only original decoration of the room that remains in it. The adjacent library room is used to explain what happened to the tapestry room;[17] the former library was designed by Adam, and was dismantled except for the marble fireplace.[10]
At the west side of the building is a long gallery,[10] which was designed by Robert Adam and installed between 1761 and 1766. It is the best preserved of the original interior (little of the rest has survived in situ).[1] It has an octagonal panelled ceiling, and plaster reliefs of griffins. A half-hexagonal bay faces the garden. The room also contains a marble caryatid fireplace designed by J Wilton.[10] As of 2016, modern sculptures are displayed in empty niches along the Long Gallery
wikipedia
USAF MC-130J demonstrating its air refuelling capability with a Bell-Boeing CV-22B Osprey at RIAT 2023.
Taken at Stowe Park, Buckinghamshire, the original gardens of Stowe House, now a school. The gardens were designed by Capability Brown.
Two Lockheed Martin F-35B Lightning II fighter jets have successfully landed on board HMS Queen Elizabeth for the first time, laying the foundations for the next 50 years of fixed wing aviation in support of the UK’s Carrier Strike Capability.
Royal Navy Commander, Nathan Gray, 41, made history by being the first to land on board HMS Queen Elizabeth, carefully maneuvering his stealth jet onto the thermal coated deck. He was followed by Royal Navy Squadron Leader Andy Edgell, RAF, both of whom are test pilots, operating with the Integrated Test Force (ITF) based at Naval Air Station Patuxent River, Maryland.
Shortly afterwards, once a deck inspection has been conducted and the all-clear given, Cmdr Gray became the first pilot to take off using the ship’s ski-ramp.
From Wikipedia, the free encyclopedia
The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, all-weather, stealth, fifth-generation, multirole combat aircraft, designed for ground-attack and air-superiority missions. It is built by Lockheed Martin and many subcontractors, including Northrop Grumman, Pratt & Whitney, and BAE Systems.
The F-35 has three main models: the conventional takeoff and landing F-35A (CTOL), the short take-off and vertical-landing F-35B (STOVL), and the catapult-assisted take-off but arrested recovery, carrier-based F-35C (CATOBAR). The F-35 descends from the Lockheed Martin X-35, the design that was awarded the Joint Strike Fighter (JSF) program over the competing Boeing X-32. The official Lightning II name has proven deeply unpopular and USAF pilots have nicknamed it Panther, instead.
The United States principally funds F-35 development, with additional funding from other NATO members and close U.S. allies, including the United Kingdom, Italy, Australia, Canada, Norway, Denmark, the Netherlands, and formerly Turkey. These funders generally receive subcontracts to manufacture components for the aircraft; for example, Turkey was the sole supplier of several F-35 parts until its removal from the program in July 2019. Several other countries have ordered, or are considering ordering, the aircraft.
As the largest and most expensive military program ever, the F-35 became the subject of much scrutiny and criticism in the U.S. and in other countries. In 2013 and 2014, critics argued that the plane was "plagued with design flaws", with many blaming the procurement process in which Lockheed was allowed "to design, test, and produce the F-35 all at the same time," instead of identifying and fixing "defects before firing up its production line". By 2014, the program was "$163 billion over budget [and] seven years behind schedule". Critics also contend that the program's high sunk costs and political momentum make it "too big to kill".
The F-35 first flew on 15 December 2006. In July 2015, the United States Marines declared its first squadron of F-35B fighters ready for deployment. However, the DOD-based durability testing indicated the service life of early-production F-35B aircraft is well under the expected 8,000 flight hours, and may be as low as 2,100 flight hours. Lot 9 and later aircraft include design changes but service life testing has yet to occur. The U.S. Air Force declared its first squadron of F-35As ready for deployment in August 2016. The U.S. Navy declared its first F-35Cs ready in February 2019. In 2018, the F-35 made its combat debut with the Israeli Air Force.
The U.S. stated plan is to buy 2,663 F-35s, which will provide the bulk of the crewed tactical airpower of the U.S. Air Force, Navy, and Marine Corps in coming decades. Deliveries of the F-35 for the U.S. military are scheduled until 2037 with a projected service life up to 2070.
Development
F-35 development started in 1992 with the origins of the Joint Strike Fighter (JSF) program and was to culminate in full production by 2018. The X-35 first flew on 24 October 2000 and the F-35A on 15 December 2006.
The F-35 was developed to replace most US fighter jets with the variants of a single design that would be common to all branches of the military. It was developed in co-operation with a number of foreign partners, and, unlike the F-22 Raptor, intended to be available for export. Three variants were designed: the F-35A (CTOL), the F-35B (STOVL), and the F-35C (CATOBAR). Despite being intended to share most of their parts to reduce costs and improve maintenance logistics, by 2017, the effective commonality was only 20%. The program received considerable criticism for cost overruns during development and for the total projected cost of the program over the lifetime of the jets.
By 2017, the program was expected to cost $406.5 billion over its lifetime (i.e. until 2070) for acquisition of the jets, and an additional $1.1 trillion for operations and maintenance. A number of design deficiencies were alleged, such as: carrying a small internal payload; performance inferior to the aircraft being replaced, particularly the F-16; lack of safety in relying on a single engine; and flaws such as the vulnerability of the fuel tank to fire and the propensity for transonic roll-off (wing drop). The possible obsolescence of stealth technology was also criticized.
Design
Overview
Although several experimental designs have been developed since the 1960s, such as the unsuccessful Rockwell XFV-12, the F-35B is to be the first operational supersonic STOVL stealth fighter. The single-engine F-35 resembles the larger twin-engined Lockheed Martin F-22 Raptor, drawing design elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, proposed for a 1972 supersonic VTOL fighter requirement for the Sea Control Ship.
Lockheed Martin has suggested that the F-35 could replace the USAF's F-15C/D fighters in the air-superiority role and the F-15E Strike Eagle in the ground-attack role. It has also stated the F-35 is intended to have close- and long-range air-to-air capability second only to that of the F-22 Raptor, and that the F-35 has an advantage over the F-22 in basing flexibility and possesses "advanced sensors and information fusion".
Testifying before the House Appropriations Committee on 25 March 2009, acquisition deputy to the assistant secretary of the Air Force, Lt. Gen. Mark D. "Shack" Shackelford, stated that the F-35 is designed to be America's "premier surface-to-air missile killer, and is uniquely equipped for this mission with cutting-edge processing power, synthetic aperture radar integration techniques, and advanced target recognition".
Improvements
Ostensible improvements over past-generation fighter aircraft include:
Durable, low-maintenance stealth technology, using structural fiber mat instead of the high-maintenance coatings of legacy stealth platforms
Integrated avionics and sensor fusion that combine information from off- and on-board sensors to increase the pilot's situational awareness and improve target identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes
High-speed data networking including IEEE 1394b and Fibre Channel (Fibre Channel is also used on Boeing's Super Hornet.
The Autonomic Logistics Global Sustainment, Autonomic Logistics Information System (ALIS), and Computerized maintenance management system to help ensure the aircraft can remain operational with minimal maintenance manpower The Pentagon has moved to open up the competitive bidding by other companies. This was after Lockheed Martin stated that instead of costing 20% less than the F-16 per flight hour, the F-35 would actually cost 12% more. Though the ALGS is intended to reduce maintenance costs, the company disagrees with including the cost of this system in the aircraft ownership calculations. The USMC has implemented a workaround for a cyber vulnerability in the system. The ALIS system currently requires a shipping-container load of servers to run, but Lockheed is working on a more portable version to support the Marines' expeditionary operations.
Electro-hydrostatic actuators run by a power-by-wire flight-control system
A modern and updated flight simulator, which may be used for a greater fraction of pilot training to reduce the costly flight hours of the actual aircraft
Lightweight, powerful lithium-ion batteries to provide power to run the control surfaces in an emergency
Structural composites in the F-35 are 35% of the airframe weight (up from 25% in the F-22). The majority of these are bismaleimide and composite epoxy materials. The F-35 will be the first mass-produced aircraft to include structural nanocomposites, namely carbon nanotube-reinforced epoxy. Experience of the F-22's problems with corrosion led to the F-35 using a gap filler that causes less galvanic corrosion to the airframe's skin, designed with fewer gaps requiring filler and implementing better drainage. The relatively short 35-foot wingspan of the A and B variants is set by the F-35B's requirement to fit inside the Navy's current amphibious assault ship parking area and elevators; the F-35C's longer wing is considered to be more fuel efficient.
Costs
A U.S. Navy study found that the F-35 will cost 30 to 40% more to maintain than current jet fighters, not accounting for inflation over the F-35's operational lifetime. A Pentagon study concluded a $1 trillion maintenance cost for the entire fleet over its lifespan, not accounting for inflation. The F-35 program office found that as of January 2014, costs for the F-35 fleet over a 53-year lifecycle was $857 billion. Costs for the fighter have been dropping and accounted for the 22 percent life cycle drop since 2010. Lockheed stated that by 2019, pricing for the fifth-generation aircraft will be less than fourth-generation fighters. An F-35A in 2019 is expected to cost $85 million per unit complete with engines and full mission systems, inflation adjusted from $75 million in December 2013.
Croome Court is a mid-18th-century Neo-Palladian mansion surrounded by extensive landscaped parkland at Croome D'Abitot, near Upton-upon-Severn in south Worcestershire, England. The mansion and park were designed by Lancelot "Capability" Brown for George Coventry, 6th Earl of Coventry, and they were Brown's first landscape design and first major architectural project. Some of the mansion's rooms were designed by Robert Adam. St Mary Magdalene's Church, Croome D'Abitot that sits within the grounds of the park is now owned and cared for by the Churches Conservation Trust.
The mansion house is owned by Croome Heritage Trust and leased to the National Trust, which operates it as a tourist attraction. The National Trust owns the surrounding parkland, which is also open to the public.
Location
Croome Court is located near to Croome D'Abitot, in Worcestershire,[1] near Pirton, Worcestershire.[2] The wider estate was established on lands that were once part of the royal forest of Horewell.[3] Traces of these older landscapes, such as unimproved commons and ancient woodlands, can be found across the former Croome Estate.[4]
House
Croome Court South Portico
History
See also: History of Worcestershire § Georgian society, politics and religion
The foundations and core of Croome Court, including the central chimney stack structure, date back to the early 1640s.[5] Substantial changes to this early house were made by Gilbert Coventry, 4th Earl of Coventry.[6]
George Coventry, the 6th Earl, inherited the estate in 1751, along with the existing Jacobean house. He commissioned Lancelot "Capability" Brown, with the assistance of Sanderson Miller, to redesign the house and estate.[7][1] It was Brown's "first flight into the realms of architecture" and a "rare example of his architectural work",[8] and it is an important and seminal work.[9] It was built between 1751 and 1752, and it and Hagley Hall are considered to be the finest examples of Neo-Palladian architecture in Worcestershire. Notable Neo-Palladian features incorporated into Croome Court include the plain exterior and the corner towers with pyramidal roofs (a feature first used by Inigo Jones in the design of Wilton House in Wiltshire).[1] Robert Adam worked on the interior of the building from 1760 onwards.[10] The house was visited by George III,[2][11] as well as by Queen Victoria[7] during summers when she was a child, and George V (when Duke of York).[11]
A jam factory was built near Pershore railway station by George Coventry, 9th Earl of Coventry in about 1880, to provide a market for Vale of Evesham fruit growers in times of surplus. Although the Croome connection with jam-making had ceased, the building was leased by the Croome Estate Trust during the First World War to the Huddersfield Fruit Preserving Company as a pulping station.[12] The First World War deeply affected Croome; there were many local casualties, although the house was not requisitioned for the war effort. This is possibly because it was the home of the Lord-lieutenant of the county, who needed a residence for his many official engagements.[13] Croome Court was requisitioned during the Second World War by the Ministry of Works, and leased for a year to the Dutch Government as a possible refuge for Queen Wilhelmina of the Netherlands to escape the Nazi occupation of the Netherlands. However, evidence shows that Queen Wilhelmina stayed for two weeks at the most, perhaps because of the noise and the fear created by the proximity of RAF Defford. The Dutch Royal family later emigrated to Canada for the duration of the war.
The Croome Estate Trust sold the Court in 1948, along with 38 acres (15 ha) of land, to the Roman Catholic Archdiocese of Birmingham, and the mansion became St Joseph's Special School, which was run by nuns[14] from 1950[11] until 1979.[14] In 1979, the hall was taken over by the International Society for Krishna Consciousness (ISKCON, the Hare Krishna movement) which used it as its UK headquarters and a training college,[15] called Chaitanya College.[14] During their tenure they repainted the Dining Room.[16] ISKCON left the estate in 1984 for financial reasons. It held a festival at the hall in 2011.[15] From 1984 onwards, various owners tried to use the property as a training centre; apartments; a restaurant and conference centre; and a hotel and golf course,[14] before once more becoming a private family home,[2][14] with outbuildings converted to private houses.[14]
The house was purchased by the Croome Heritage Trust, a registered charity,[17] in October 2007,[18] and it is now managed by the National Trust as a tourist attraction. It opened to the public in September 2009, at which point six of the rooms had been restored, costing £400,000, including the Saloon. It was estimated that another £4 million[2][19] to £4.8 million would be needed to restore the entire building. Fundraising activities for the restoration included a 2011 raffle for a Morgan sports car organised by Lord and Lady Flight. After the restoration is complete, a 999-year lease on the building will be granted to the National Trust.[20] An oral history project to record recollections about Croome was funded by the Heritage Lottery Fund.[14] As of 2009, the service wing was empty and in need of substantial repair.[21] The house was listed on 11 August 1952; it is currently Grade I listed.[10]
Exterior
The mansion is faced with Bath stone,[7] limestone ashlar, and has both north and south facing fronts. It has a basement and two stories, with three stories in the end pavilions. A slate roof, with pyramid roofs over the corner towers, tops the building, along with three pair-linked chimneys along the axis of the house.[10]
Both fronts have 11 bays, split into three central sets of three each, and one additional bay each side. The north face has a pedimented centre, with two balustraded staircases leading to a Roman Doric doorcase. The south face has a projecting Ionic tetrastyle portico and Venetian windows. It has a broad staircase, with Coade stone sphinxes on each side, leading to a south door topped with a cornice on consoles. The wings have modillion cornice and balustrade.[10]
A two-story L-shaped service wing is attached to the east side of the mansion. It is made of red brick and stone, with slate roofs.[10] It was designed by Capability Brown in 1751–1752.[21] On the far side of the service wing, a wall connects it to a stable court.[10]
Interior
The Tapestry Room, now at the Metropolitan Museum of Art
... and the Tapestry Room at Croome Court today
The interior of the house was designed partially by Capability Brown, with plasterwork by G. Vassalli, and partially by Robert Adam, with plasterwork by Joseph Rose, Jr. It has a central spine corridor. A stone staircase, with iron balusters, is at the east end.[10]
The entrance hall is on the north side of the building, and has four fluted Doric columns, along with moulded doorcases. To the east of the entrance hall is the dining room, which has a plaster ceiling and cornice, while to the west is a billiard room, featuring fielded panelling, a plaster cornice, and a rococo chimneypiece. The three rooms were probably decorated around 1758–1759 by Capability Brown.[10] The dining room was vibrantly repainted by the Hare Krishnas in the 1970s-80s.[16]
The central room on the south side is a saloon, probably by Brown and Vassalli. It has an elaborate ceiling, with three panels, deep coving, and a cornice, along with two Ionic chimneypieces, and Palladian doorcases.[22] King George III was entertained by George Coventry, the 6th Earl, in the house's Saloon.[2] A drawing room is to the west of the saloon, and features rococo plasterwork and a marble chimneypiece.[10]
To the east of the saloon is the Tapestry Room.[10] This was designed in 1763–1771, based on a design by Robert Adam, and contained tapestries and furniture covers possibly designed by François Boucher and Maurice Jacques, and made by Manufacture Nationale des Gobelins.[23] Around 1902 the 9th Earl sold the tapestries and seating to a Parisian dealer. The Samuel H. Kress Foundation purchased the ceiling, floor, chimneypiece, chair rails, doors and door surrounds in 1949; they were donated to the Metropolitan Museum of Art, New York, in 1958. In 1959, the Kress Foundation also helped the Metropolitan Museum acquire the chair and sofa frames, which they recovered using the original tapestry seats.[7][23] A copy of the ceiling was installed in place of the original.[10] As of 2016, the room is displayed as it would have looked after the tapestries had been sold, with a jug and ewer on display as the only original decoration of the room that remains in it. The adjacent library is used to explain what happened to the tapestry room;[16] the former library was designed by Adam, and was dismantled except for the marble chimneypiece.[10]
At the west side of the building is a Long Gallery[10] which was designed by Robert Adam and installed between 1761 and 1766. It is the best preserved element of the original interior (little of the rest has survived in situ).[1] It has an octagonal panelled ceiling, and plaster reliefs of griffins. A half-hexagonal bay faces the garden. The room also contains a marble caryatid chimneypiece designed by J Wilton.[10] As of 2016, modern sculptures are displayed in empty niches along the Long Gallery....Wikipedia
Another consignment of South Wales coal for the Lafarge Cement Works at Westbury was recorded at Severn Tunnel Junction in the care of EWS 60002 'Capability Brown'. The MFO 6C79 from Parc Slip would travel via Bath and the Avon Valley to reach Hawkeridge Junction.
All images on this site are exclusive property and may not be copied, downloaded, reproduced, transmitted, manipulated or used in any way without expressed written permission of the photographer. All rights reserved – Copyright Don Gatehouse
Temple Newsam (historically Temple Newsham), (grid reference SE357322) is a Tudor-Jacobean house in Leeds, West Yorkshire, England, with grounds landscaped by Capability Brown.
The estate lends its name to the Temple Newsam ward of Leeds City Council, in which it is situated, and lies to the east of the city, just south of Halton Moor, Halton, Whitkirk and Colton. It is one of nine sites in the Leeds Museums & Galleries group.
The house is a Grade I listed building, defined as a "building of outstanding or national architectural or historic interest". The stables are Grade II* listed ("particularly significant buildings of more than local interest"), and ten separate features of the estate are Grade II listed ("buildings of special architectural or historic interest"), including the Sphinx Gates and the Barn.[1] Temple Newsam House is one of Leeds Museums and Galleries sites.[2] It is also part of the research group, Yorkshire Country House Partnership.[3]
History
1066 to 1520
In the Domesday Book of 1086 the manor is listed as Neuhusam (meaning new houses) and was held by Ilbert de Lacy and his sons.[4] Before the Norman Conquest of 1066 it had been held by Dunstan and Glunier, Anglo-Saxon thanes.[4] In about 1155, Henry de Lacy gave it to the Knights Templar, who built Temple Newsam Preceptory on a site near the present house.[5] The Templars farmed the estate very efficiently, with 1100 animals.[6] In 1307 the Templars were suppressed, and Edward II granted the manor to Sir Robert Holland who held it until 1323 when he was deprived of his estates.[6] The Templars tried to retake the estate but they were forced to surrender and in 1327 it was granted to Mary de St Pol, the Countess of Pembroke, who held the manor for 50 years.[6] In 1377 by royal decree the estate reverted to Philip Darcy, 4th Baron Darcy de Knayth (1341–1398).[6] It then passed through several members of the Darcy family, until it was inherited by the 21-year old Thomas, Lord Darcy in 1488.[7] Between 1500 and 1520 a Tudor manor house, known as Temple Newsam House, was built on the site.[8] It has also been spelled "Newsham" in the past.[9]
An oil on panel painting by Hans Eworth of Henry Stuart and his brother Charles Stuart in a grand interior based on a print by Hans Vreedman de Vries
An oil on panel painting from 1563 by Hans Eworth of Henry Stuart and his brother Charles Stuart in a grand interior based on a print by Hans Vreedman de Vries which may reflect Temple Newsam's Great Chamber
1500 to 1650
In 1537 Thomas, Lord Darcy was executed for the part he played in the Pilgrimage of Grace and the property was seized by the Crown.[7] In 1544 Henry VIII gave it to his niece Lady Margaret Douglas (Countess of Lennox), and she lived there with her husband Matthew Stewart, 4th Earl of Lennox.[7] Their son Henry Stuart, Lord Darnley, who was born in the house in 1545 and educated there, married Mary, Queen of Scots, by whom he was the father of King James VI of Scotland and I of England.[10] A portrait of Henry and his brother was probably intended to represent the interior of Temple Newsam despite being based on a print of an ideal interior.[11] Following the marriage in 1565, Temple Newsam was seized by Queen Elizabeth I and was managed by an agent.[12]
In 1609 King James I, successor to Elizabeth, granted the estate to his Franco-Scottish second cousin Ludovic Stewart, 2nd Duke of Lennox (1574–1624), who was a favourite of the King and given many titles and estates, including farmland and coalmines in the local area.[13] Despite his opportunities, Ludovic was in constant debt and he mortgaged the estate in 1614 for the sum of £9,000 (around £860,000 in today's money).[14] In 1622 Lennox began the sale of the estate to Sir Arthur Ingram (c. 1565 – 1642), a Yorkshire-born London merchant, civil servant, investor in colonial ventures and arms dealer, for £12,000, which he paid in two instalments, the last in July 1624, after Lennox's death.[14] During the next 20 years the mansion was rebuilt, incorporating some of the previous house in the west wing.[8] The north and south wings were rebuilt and the east wing was demolished after a bad fire in 1635.[15] Arthur's son, also called Arthur, inherited the estate with its debts and continued the building and renovation work.[16] Six months after Charles I was beheaded in 1649, Arthur Ingram the younger was declared delinquent and he compounded his estates and retired to Temple Newsam.[17]
1650 to 1900
After the death of Arthur the younger's eldest son, Thomas, in 1660, Temple Newsam was inherited by Arthur's second son, Henry Ingram, 1st Viscount of Irvine (created a peer of Scotland as Baron Ingram and Viscount of Irvine in 1661 - although the family used the English form "Irwin").[18] In 1661, Henry married Lady Essex Montagu, daughter of Edward Montagu, 2nd Earl of Manchester, a favourite of Charles II.[18] The estate then passed through Henry's two sons and five grandsons, the last being Henry Ingram, 7th Viscount of Irvine.[18] The 4th Viscount brought back paintings from his Grand Tour of 1704-7.[19] Extant receipts from 1692 show women as well as men were employed to work the estate in haymaking.[20] In 1712, William Etty designed a new approach to the house, with a bridge and ponds.[21][22] In 1714, Temple Newsam was inherited by Rich Ingram, the 5th Viscount, and his wife Ann who spent a vast fortune furnishing the house and creating the East Avenue.[19] Between 1738 and 1746, Henry Ingram, 7th Viscount of Irvine remodelled the west and north wings of the house, creating new bedrooms and dressing rooms and the picture gallery.[23] A painting in Leeds City Art Gallery by Philippe Mercier of c. 1745 shows Henry and his wife standing in front of Temple Newsam House.[24]
A coloured engraving made in 1699 by J Kip after a drawing by Leonard Knyff showing an aerial view of the house and estate at Temple Newsam
1699 Engraving by J Kip after a drawing by Leonard Knyff
In the 1760s, Charles Ingram, 9th Viscount of Irvine, employed Capability Brown to re-landscape the park on the insistence of his wife, Frances Shepheard, daughter of Samuel Shepheard.[25] Reflecting her interest in pastoral landscape design, Frances is depicted as a shepherdess in a portrait by Benjamin Wilson at Temple Newsam.[25] Both Frances and Charles were actively involved in the design and implementation.[26] Some aspects of Brown's plan depicted in paintings by James Chapman and Michael Angelo Rooker were never completed such as a large lake near the house.[26] Extant financial records show that in 1759 women as well as men were employed as garden labourers.[20] After Charles died in 1778, Frances rebuilt the south wing in 1796; she lived at Temple Newsam until her death in 1807.[27] Charles and Frances's eldest daughter Isabella Ingram, (Marchioness of Hertford) (d.1834) who inherited Temple Newsam, was the mistress of the Prince of Wales (later King George IV) from 1806 to 1819. In 1806, George visited Temple Newsam and presented Isabella with Chinese wallpaper, which she hung in the small Drawing Room next to the Great Hall in around 1820, embellished with cut out birds from Audubon's The Birds of America (now worth £7.5 million).[28] Lady Hertford inherited the house in 1807; after her husband died in 1822 she spent the season in London, and the rest of the time at Temple Newsam where she involved herself in charitable works including distributing food and clothing to the local people.[29] She allowed the servants to hold an annual supper and ball at Temple Newsam.[29] Reports of poachers were made during 1826 and 1827.[30] During the last years of Isabella's life, the canal, railway and roads encroached on the estate as well as coal mining; and she dealt with the companies setting these up.[29] In 1820 the novelist Sir Walter Scott published Ivanhoe featuring a Templar preceptory named Temple Stowe, believed to have been modelled on Temple Newsam; the name is preserved in local road names such as Templestowe Crescent.[31] At her death in 1834, Isabella left Temple Newsam to her widowed sister, Frances Ingram Shepheard, wife of Lord William Gordon, who died in 1841.[32]
Temple Newsam House from Morris's Country Seats (1880)
In 1841 the estate was inherited by Hugo Charles Meynell Ingram (d. 1869), son of Elizabeth Ingram, sister of Frances Ingram (Lady Gordon), who made no alterations to the estate.[33] In 1868, the Prince of Wales stayed at Temple Newsam during his visit to Leeds to open the Fine Art Exhibition in the New Infirmary; temporary triumphal arches were erected on the estate.[34] Following Hugo Charles's death, his son Hugo Meynell-Ingram (d.1871) inherited Temple Newsam; two years later, at his death, his wife Emily Meynell Ingram (d.1904) inherited the estate.[33] Emily spent a large part of her widowhood at Temple Newsam; she developed it considerably by replacing the sash windows and remodelling the dining room, great staircase and Lord Darnley's room.[33] Emily bequeathed Temple Newsam to her nephew Edward Wood, 1st Earl of Halifax.[8]
20th century
In 1909, 610 acres (2.5 km2) of the estate at Knostrop were compulsorily purchased by Leeds Corporation to build a sewage plant.[35] During the First World War (1914–17) the south wing of the house was turned into a hospital by Edward Wood and his wife Dorothy. Edward Wood fought in France as part of the Yorkshire Hussars, whilst Dorothy oversaw the running of the hospital as part of the Mayors War Committee.[36] In 1922 Edward Wood sold the park and house to Leeds Corporation for a nominal sum, placing covenants over them to ensure their preservation for the future.[35]
On 19 October 1923, Temple Newsam was opened to the public along with a golf course.[37] In the Derby Daily Telegraph newspaper, Temple Newsam was compared to Hampton Court.[37] Despite many people visiting the house and using the golf course, the Corporation lost money during the first decade mostly due to poor farming practices.[37] In July 1932, the Great Yorkshire Show was held at Temple Newsam and was a great success.[37] Preparations for war were made as early as April 1939, and in August, small items were being packed up for storage.[37] In September 1939, Temple Newsam was closed to the public and items were moved there for storage from Leeds City Art Gallery.[37] It was decided that objects would be displayed, and the house was officially reopened in November 1939, when it was again likened to Hampton Court in the press.[37]
Architecture
Photograph of entrance porch of Temple Newsam House, Leeds, showing at top the word 'FATHER', below a mullioned window, below a raised portico with coat of arms above a doorway flanked by two Ionic columns on each side.
Entrance Porch 17th century
Photograph of the west front of Temple Newsam
Centre of Temple Newsam west front
Remains of the early 16th century house were retained in the new building, including the brickwork and bay windows in the centre of the west front.[38] The plan of the new house was a conservative E-shape.[38] The Long Gallery and entrance hall in the south wing followed Elizabethan and early Jacobean styles.[38] The entrance porch has Classical columns but they are of Flemish design, rather than following correct Italian design.[38] There are Tudor doorways and timberwork in the cellars, which are largely Tudor in date.[39] Tudor features have also been discovered beneath later layers of decoration, including Lord Darcy's crest scratched into the plaster in the Blue Damask room.[40] An inventory of 1565 indicates that the hall, great chamber (later the dining room), gallery and chapel (later the kitchen) were probably where they are now.[40] There is a Tudor doorway in the north wing which was probably the entrance to the original chapel.[41]
In the 17th century, the south and north wings were rebuilt and the east wing demolished, replaced by a low wall with an arched gateway, giving the house a fashionable 'half-H' appearance.[39] It is possible that the man who made plans for the alteration was Bernard Dinninghof of York.[41] There is also some resemblance to designs by Inigo Jones.[42] Round the top of the house, letters appear in a balustrade, declaring the piety and loyalty of Sir Arthur Ingram: 'ALL GLORY AND PRAISE BE GIVEN TO GOD THE FATHER THE SON AND HOLY GHOST ON HIGH PEACE ON EARTH GOOD WILL TOWARDS MEN HONOUR AND TRUE ALLEGIANCE TO OUR GRACIOUS KING LOVING AFFECTION AMONGST HIS SUBJECTS HEALTH AND PLENTY BE WITHIN THIS HOUSE.'[38] The chapel in the north wing retains some 17th century features, such as armorial stained glass, probably by Henry Gyles and a carved wooden pulpit by Thomas Ventris, made around 1636, with geometric patterns, pilasters and friezes.[38] The walls had panels of Old Testament figures, painted by John Carleton.[38] An inventory dated 1667 records that the House had 66 rooms and 11 outhouses.[39] An engraving by Kip and Knyff dated 1699 is an accurate representation of the house, showing the varying height of the house and some buildings that were later demolished, including the arched gateway flanked by two small lodges and a detached garden building dating from the mid 1670s.[23]
Photograph of stone and brick Sphinx gate piers at Temple Newsam, c. 1760 by Lancelot Brown based on designs published by Lord Burlington in 1738 and used at Chiswick
Sphinx gate piers, c. 1760
Photograph of the mid-18th century stable block at Temple Newsam showing the pediment
Stable Block at Temple Newsam, added by Henry, 7th Lord Irwin
In 1718, the steward of Temple Newsam suggested an underground service passage to link the north and south wings to the 5th Viscount, who agreed.[43] This tunnel linked the original kitchens in the south wing to the rest of the house.[44] In 1738, Henry, 7th Viscount Irwin wrote to his mother describing the neglected state of the house with windows coming away and cracked brickwork.[23] The house was almost entirely remodelled by Henry.[38] He wanted to follow Palladian design and used craftsmen from York to do so.[45] He widened the gallery, improved the ceiling and windows and created additional rooms.[23] The gallery, completed around 1746, has fine Rococo carvings with overmantle paintings of classical scenes by Antonio Joli.[19] There are also elaborate gilded Rococo ornamental candle holders.[19] The gallery ceiling has detailed stucco work including a medallion of King George I.[19] The ceilings in the new Saloon and Library, made from the old Long Gallery, were decorated by Thomas Perritt and Joseph Rose.[45] The doorcases are elaborately carved, probably by Richard Fisher.[45] Two chimney pieces in the Saloon were based on designs by William Kent.[45] The distinctive sphinx gate piers by Lancelot Brown constructed in 1768 were based on designs published by Lord Burlington in 1738 and used at Chiswick.[45][1] The main rooms in the west wing were redecorated and the windows were replaced with sliding sash windows.[45] A large pedimented stable block was built to the north of the house, in 1742 and probably designed by Daniel Garratt, also in the Palladian style.[45][46] A painting by Mercier of around 1749, also shows a planned block to the south and a low wall connecting the north and south wings which were never completed.[23][21]
In 1796, Frances Shepheard employed a Mr Johnson to alter and reface the south wing in a style which tried to copy that of Sir Arthur Ingram's original house.[45] Her approach was a departure from the designs for the wing commissioned by her dead husband from John Carr and Robert Adam, as well as the landscaping by Capability Brown who was also consulted about rebuilding the south wing.[45] The wing was made two storeys high throughout with a suite of reception rooms on the ground floor with state bedchambers above.[27] In the 1790s, the kitchens were moved to the north wing and the original kitchen became a brushing room where servants brushed down nobles returning from hunting parties.[44]
At the end of the 19th century, Emily Meynell Ingram replaced the sash windows with stone mullions and leaded lights and rebuilt the north porch adding the Meynell Ingram coat of arms over the doorway.[27] She redecorated several rooms and had the great oak staircase installed.[27] The dining room, great staircase and Lord Darnley's room were remodelled in Elizabethan style.[33] In 1877, Emily converted the library at the east end of the gallery into a chapel.[47]
Coalmining on the estate
Estate records show the existence of coal pits in and around the park in the seventeenth century and Bell Wood to the south of the house would have had bell pits for coal extraction. A colliery at Halton village was leased to a number of different individuals from 1660 through to at least the 1790s. The leases generally required the leaseholder to supply coals to Temple Newsam house.[48]
In 1815, William Fenton, one of the 'Coal Kings' of Yorkshire,[49] began the sinking of a mine shaft on the estate at Thorpe Stapleton. The colliery was named Waterloo to commemorate the famous battle of that year.[50] Waterloo Colliery was operated as a royalty concession with contracted 'rents' for coal extracted going to the Temple Newsam landowner. Fenton also had a village built for his workers on land between the River Aire and the Aire and Calder navigation. The village was initially called Newmarket but then became Irwin Square on ordnance survey maps[51] and Ingram Place on census lists, but it was commonly simply known as Waterloo. The Yorkshire, Lancashire and England cricketer Albert Ward was born here in 1865. The village had two rows of cottages and a school building. It was connected to the colliery by a wooden footbridge over the river.[52] Deep coal mining on the estate ended with the closure of the Temple Pit of Waterloo Main Colliery in 1968.
Temple Newsam House
Opencast mining on the estate began in May 1942. Seven sites were exploited to the south of the house almost entirely destroying Capability Brown's landscape. One site reached within 330 feet (100 m) of the South Terrace. It continued at the Gamblethorpe site as far as Dawson's Wood, in full view of the house, until 1987.[53] No trace of the opencast remains now as the parkland was re-landscaped.
In 2019 there was a temporary exhibition about coal mining at Temple Newsam which was called 'Blot on the Landscape'.[54]
House and estate today
The house and estate are owned by Leeds City Council and open to the public. The house has undergone substantial restoration to its exterior. There is an established programme of restoring rooms back to known previous configurations, reversing the numerous intrusive installations and modifications that took place during the building's "art museum" phase.
The wider estate is made up of woods (the second largest part of the Forest of Leeds).[55] There are sporting facilities for football, golf, running, cycling, horse-riding and orienteering. There is an innovative children's playground opened in 2011 which caters for both disabled and able-bodied children.[56] Pegasus Wood, to the south of the house, commemorates veterans of the Normandy Landing at Pegasus Bridge in 1944.[57]
Photograph of brick barn at the Home Farm, Temple Newsam
Great Barn, Home Farm, Temple Newsam
The Home Farm, open to the public, has a barn built in 1694 and is the largest working rare breeds farm in Europe, and only one of 16 nationally approved by the Rare Breeds Survival Trust. Breeds include Gloucester, Kerry, Irish Moiled, Red Poll, White Park, British White, Beef Shorthorn, Vaynol and Belted Galloway cattle; Kerry Hill; Whitefaced Woodland and Portland sheep, and Golden Guernsey goats.[58] The farm was targeted by arsonists twice in 2011 with damage caused to buildings, and some animals killed.[59]
There are extensive gardens, with a celebrated rhododendron walk and six national plant collections: Aster novi-belgii (Michaelmas daisies), Phlox paniculata, Delphinium elatum (Cultivars), Solenostemon scutellarioides (sys. Coleus blumei), Primula auricula and Chrysanthemum (Charm and Cascade cultivars).[60] Within the Walled Garden there are 800 yards of herbaceous borders.[61]
Collections
There are substantial holdings of fine and decorative art which are designated by the Department of Culture, Media and Sport (DCMS) as being of national significance.[62]
Of most significant historical and cultural interest is the Chippendale Society collection of Chippendale works that are on permanent loan.[63] In his book "Britain's Best Museums and Galleries", Mark Fisher (a former DCMS minister) gave the museum an excellent review. When interviewed on Front Row, Radio 4, November 2004 Fisher placed Temple Newsam House in the top three non-national museums in the country, along with Birmingham's Barber Institute and the Dulwich Picture Gallery.[64]
Ugbrooke House
Ugbrooke House is a stately home in the parish of Chudleigh, Devon, England, situated in a valley between Exeter and Newton Abbot.
It dates back over 900 years, having featured in the Domesday Book. Before the Reformation the land belonged to the Church and the house was occupied by Precentors to the Bishop of Exeter. It has been the seat of the Clifford family for over four hundred years, and the owners have held the title Baron Clifford of Chudleigh since 1672.
The 9th Baron Clifford was an aide-de-camp to Edward VII and entertained royalty, both Edward VII and George V, at Ugbrooke Park.
The house, now a Grade I listed building, was remodelled by Robert Adam, while the grounds were redesigned by Capability Brown in 1761.The grounds featured what were possibly the earliest plantings of the European White Elm Ulmus laevis in the UK.The gardens are now Grade II* listed in the National Register of Historic Parks and Gardens.[4] The house and gardens are open to the public for a limited number of days each summer.
Baron Clifford of Chudleigh
Baron Clifford of Chudleigh, of Chudleigh in the County of Devon, is a title in the Peerage of England. It was created in 1672 for Thomas Clifford. The title was created as "Clifford of Chudleigh" rather than simply "Clifford" to differentiate it from several other Clifford Baronies previously created for members of this ancient family, including the Barony of de Clifford (1299), which is extant but now held by a branch line of the Russell family, having inherited through several female lines.
Baron Clifford of Chudleigh is the major surviving male representative of the ancient Norman family which later took the name de Clifford which arrived in England during the Norman Conquest of 1066, feudal barons of Clifford, first seated in England at Clifford Castle in Herefordshire, created Baron de Clifford by writ in 1299. The family seat is Ugbrooke Park, near Chudleigh, Devon.
Notable members of this branch of the Clifford family include antiquarian Arthur Clifford (grandson of the 3rd Baron), Victoria Cross recipient Sir Henry Hugh Clifford (son of the 7th Baron), Catholic clergyman William Clifford (son of the 7th Baron) and colonial administrators Sir Bede Clifford (son of the 10th Baron) and Sir Hugh Clifford (grandson of the 7th Baron). The family is also related to the notable recusant Weld family, of Lulworth Castle, through the 7th Baron's marriage to the daughter of Cardinal Thomas Weld.
Barons Clifford of Chudleigh (1672)
Thomas Clifford, 1st Baron Clifford of Chudleigh (1630–1673)
Hugh Clifford, 2nd Baron Clifford of Chudleigh (1663–1730)
Hugh Clifford, 3rd Baron Clifford of Chudleigh (1700–1732)
Hugh Clifford, 4th Baron Clifford of Chudleigh (1726–1783)
Hugh Edward Henry Clifford, 5th Baron Clifford of Chudleigh (1756–1793)
Charles Clifford, 6th Baron Clifford of Chudleigh (1759–1831)
Hugh Charles Clifford, 7th Baron Clifford of Chudleigh (1790–1858)
Charles Hugh Clifford, 8th Baron Clifford of Chudleigh (1819–1880)
Lewis Henry Hugh Clifford, 9th Baron Clifford of Chudleigh (1851–1916)
William Hugh Clifford, 10th Baron Clifford of Chudleigh (1858–1943)
Charles Oswald Hugh Clifford, 11th Baron Clifford of Chudleigh (1887–1962)
Lewis Joseph Hugh Clifford, 12th Baron Clifford of Chudleigh (1889–1964)
Lewis Hugh Clifford, 13th Baron Clifford of Chudleigh (1916–1988)
Thomas Hugh Clifford, 14th Baron Clifford of Chudleigh (b. 1948)
The heir apparent is the present holder's son Hon. Alexander Thomas Hugh Clifford (b. 1985)
From Wikipedia, the free encyclopedia
+++ DISCLAIMER +++
Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!
Some background:
After the success of the Soviet Union’s first carrier ship, the Moskva Class (Projekt 1123, also called „Кондор“/„Kondor“) cruisers in the mid 1960s, the country became more ambitious. This resulted in Project 1153 Orel (Russian: Орёл, Eagle), a planned 1970s-era Soviet program to give the Soviet Navy a true blue water aviation capability. Project Orel would have resulted in a program very similar to the aircraft carriers available to the U.S. Navy. The ship would have been about 75-80,000 tons displacement, with a nuclear power plant and carried about 70 aircraft launched via steam catapults – the first Soviet aircraft carrier that would be able to deploy fixed-wing aircraft.
Beyond this core capability, the Orel carrier was designed with a large offensive capability with the ship mounts including 24 vertical launch tubes for anti-ship cruise missiles. In the USSR it was actually classified as the "large cruiser with aircraft armament".
Anyway, the carrier needed appropriate aircraft, and in order to develop a the aircraft major design bureaus were asked to submit ideas and proposals in 1959. OKB Yakovlev and MiG responded. While Yakovlev concentrated on the Yak-36 VTOL design that could also be deployed aboard of smaller ships without catapult and arrester equipment, Mikoyan-Gurevich looked at navalized variants of existing or projected aircraft.
While land-based fighters went through a remarkable performance improvement during the 60ies, OKB MiG considered a robust aircraft with proven systems and – foremost – two engines to be the best start for the Soviet Union’s first naval fighter. “Learning by doing”, the gathered experience would then be used in a dedicated new design that would be ready in the mid 70ies when Project 1153 was ready for service, too.
Internally designated “I-SK” or “SK-01” (Samolyot Korabelniy = carrier-borne aircraft), the naval fighter was based on the MiG-19 (NATO: Farmer), which had been in production in the USSR since 1954.
Faster and more modern types like the MiG-21 were rejected for a naval conversion because of their poor take-off performance, uncertain aerodynamics in the naval environment and lack of ruggedness. The MiG-19 also offered the benefit of relatively compact dimensions, as well as a structure that would carry the desired two engines.
Several innovations had to be addresses:
- A new wing for improved low speed handling
- Improvement of the landing gear and internal structures for carrier operations
- Development of a wing folding mechanism
- Integration of arrester hook and catapult launch devices into the structure
- Protection of structure, engine and equipment from the aggressive naval environment
- Improvement of the pilot’s field of view for carrier landings
- Improved avionics, esp. for navigation
Work on the SK-01 started in 1960, and by 1962 a heavily redesigned MiG-19 was ready as a mock-up for inspection and further approval. The “new” aircraft shared the outlines with the land-based MiG-19, but the nose section was completely new and shared a certain similarity to the experimental “Aircraft SN”, a MiG-17 derivative with side air intakes and a solid nose that carried a. Unlike the latter, the cockpit had been moved forward, which offered, together with an enlarged canopy and a short nose, an excellent field of view for the pilot.
On the SK-01 the air intakes with short splitter plates were re-located to the fuselage flanks underneath the cockpit. In order to avoid gun smoke ingestion problems (and the lack of space in the nose for any equipment except for a small SRD-3 Grad gun ranging radar, coupled with an ASP-5N computing gun-sight), the SK-01’s internal armament, a pair of NR-30 cannon, was placed in the wing roots.
The wing itself was another major modification, it featured a reduced sweep of only 33° at ¼ chord angle (compared to the MiG-19’s original 55°). Four wing hardpoints, outside of the landing gear wells, could carry a modest ordnance payload, including rocket and gun pods, unguided missiles, iron bombs and up to four Vympel K-13 AAMs.
Outside of these pylons, the wings featured a folding mechanism that allowed the wing span to be reduced from 10 m to 6.5 m for stowage. The fin remained unchanged, but the stabilizers had a reduced sweep, too.
The single ventral fin of the MiG-19 gave way to a fairing for a massive, semi-retractable arrester hook, flanked by a pair of smaller fins. The landing gear was beefed up, too, with a stronger suspension. Catapult launch from deck was to be realized through expandable cables that were attached onto massive hooks under the fuselage.
The SK-01 received a “thumbs up” in March 1962 and three prototypes, powered by special Sorokin R3M-28 engines, derivatives of the MiG-19's RB-9 that were adapted to the naval environment, were created and tested until 1965, when the type – now designated MiG-SK – went through State Acceptance Trials, including simulated landing tests on an “unsinkalble carrier” dummy, a modified part of the runway at Air Base at the Western coast of the Caspian Sea. Not only flight tests were conducted at Kaspiysk, but also different layouts for landing cables were tested and optimized as well. Furthermore, on a special platform at the coast, an experimental steam catapult went through trials, even though no aircraft starts were made from it – but weights hauled out into the sea.
Anyway, the flight tests and the landing performance on the simulated carrier deck were successful, and while the MiG-SK (the machine differed from the MiG-19 so much that it was not recognized as an official MiG-19 variant) was not an outstanding combat aircraft, rather a technology carrier with field use capabilities.
The MiG-SK’s performance was good enough to earn OKB MiG an initial production run of 20 aircraft, primarily intended for training and development units, since the whole infrastructure and procedures for naval aviation from a carrier had to be developed from scratch. These machines were built at slow pace until 1968 and trials were carried out in the vicinity of the Black Sea and the Caspian Sea.
The MiG-SK successfully remained hidden from the public, since the Soviet Navy did not want to give away its plans for a CTOL carrier. Spy flights of balloons and aircraft recognized the MiG-SK, but the type was mistaken as MiG-17 fighters. Consequently, no NATO codename was ever allocated.
Alas, the future of the Soviet, carrier-borne fixed wing aircraft was not bright: Laid down in in 1970, the Kiev-class aircraft carriers (also known as Project 1143 or as the Krechyet (Gyrfalcon) class) were the first class of fixed-wing aircraft carriers to be built in the Soviet Union, and they entered service, together with the Yak-38 (Forger) VTOL fighter, in 1973. This weapon system already offered a combat performance similar to the MiG-SK, and the VTOL concept rendered the need for catapult launch and deck landing capability obsolete.
OKB MiG still tried to lobby for a CTOL aircraft (in the meantime, the swing-wing MiG-23 was on the drawing board, as well as a projected, navalized multi-purpose derivative, the MiG-23K), but to no avail.
Furthermore, carrier Project 1153 was cancelled in October 1978 as being too expensive, and a program for a smaller ship called Project 11435, more V/STOL-aircraft-oriented, was developed instead; in its initial stage, a version of 65,000 tons and 52 aircraft was proposed, but eventually an even smaller ship was built in the form of the Kuznetsov-class aircraft carriers in 1985, outfitted with a 12-degree ski-jump bow flight deck instead of using complex aircraft catapults. This CTOL carrier was finally equipped with navalized Su-33, MiG-29 and Su-25 aircraft – and the MiG-SK paved the early way to these shipboard fighters, especially the MiG-29K.
General characteristics:
Crew: One
Length: 13.28 m (43 ft 6 in)
Wingspan: 10.39 m (34 ft)
Height: 3.9 m (12 ft 10 in)
Wing area: 22.6 m² (242.5 ft²)
Empty weight: 5.172 kg (11,392 lb)
Max. take-off weight: 7,560 kg (16,632 lb)
Powerplant:
2× Sorokin R3M-28 turbojets afterburning turbojets, rated at 33.8 kN (7,605 lbf) each
Performance:
Maximum speed: 1,145 km/h (618 knots, 711 mph) at 3,000 m (10,000 ft)
Range: 2,060 km (1,111 nmi, 1,280 mi) with drop tanks
Service ceiling: 17,500 m (57,400 ft)
Rate of climb: 180 m/s (35,425 ft/min)
Wing loading: 302.4 kg/m² (61.6 lb/ft²)
Thrust/weight: 0.86
Armament:
2x 30 mm NR-30 cannons in the wing roots with 75 RPG
4x underwing pylons, with a maximum load of 1.000 kg (2.205 lb)
The kit and its assembly:
This kitbash creation was spawned by thoughts concerning the Soviet Naval Aviation and its lack of CTOL aircraft carriers until the 1980ies and kicked-off by a CG rendition of a navalized MiG-17 from fellow member SPINNERS at whatifmodelers.com, posted a couple of months ago. I liked this idea, and at first I wanted to convert a MiG-17 with a solid nose as a dedicated carrier aircraft. But the more I thought about it and did historic research, the less probable this concept appeared to me: the MiG-17 was simply too old to match Soviet plans for a carrier ship, at least with the real world as reference.
A plausible alternative was the MiG-19, esp. with its twin-engine layout, even though the highly swept wings and the associated high start and landing speeds would be rather inappropriate for a shipborne fighter. Anyway, a MiG-21 was even less suitable, and I eventually took the Farmer as conversion basis, since it would also fit into the historic time frame between the late 60ies and the mid-70ies.
In this case, the basis is a Plastyk MiG-19 kit, one of the many Eastern European re-incarnations of the vintage KP kit. This cheap re-issue became a positive surprise, because any former raised panel and rivet details have disappeared and were replaced with sound, recessed engravings. The kit is still a bit clumsy, the walls are very thick (esp. the canopy – maybe 2mm!), but IMHO it’s a considerable improvement with acceptable fit, even though there are some sink holes and some nasty surprises (in my case, for instance, the stabilizer fins would not match with the rear fuselage at all, and you basically need putty everywhere).
Not much from the Plastyk kit was taken over, though: only the fuselage’s rear two-thirds were used, some landing gear parts as well as fin and the horizontal stabilizers. The latter were heavily modified and reduced in sweep in order to match new wings from a Hobby Boss MiG-15 (the parts were cut into three pieces each and then set back together again).
Furthermore, the complete front section from a Novo Supermarine Attacker was transplanted, because its short nose and the high cockpit are perfect parts for a carrier aircraft. The Attacker’s front end, including the air intakes, fits almost perfectly onto the round MiG-19 forward fuselage, only little body work was necessary. A complete cockpit tub and a new seat were implanted, as well as a front landing gear well and walls inside of the (otherwise empty) air intakes. The jet exhausts were drilled open, too, and afterburner dummies added. Simple jobs.
On the other side, the wings were trickier than expected. The MiG-19 kit comes with voluminous and massive wing root fairings, probably aerodynamic bodies for some area-ruling. I decided to keep them, but this caused some unexpected troubles…
The MiG-15 wings’ position, considerably further back due to the reduced sweep angle, was deduced from the relative MiG-19’s landing gear position. A lot of sculpting and body work followed, and after the wings were finally in place I recognized that the aforementioned, thick wing root fairings had reduced the wing sweep – basically not a bad thing, but with the inconvenient side effect that the original wing MiG-15 fences were not parallel to the fuselage anymore, looking rather awkward! What to do? Grrrr…. I could not leave it that way, so I scraped them away and replaced with them with four scratched substitutes (from styrene profiles), moving the outer pair towards the wing folding mechanism.
Under the wings, four new pylons were added (two from an IAI Kfir, two from a Su-22) and the ordnance gathered from the scrap box – bombs and rocket pods formerly belonged to a Kangnam/Revell Yak-38.
The landing gear was raised by ~2mm for a higher stance on the ground. The original, thick central fin was reduced in length, so that it could become a plausible attachment point for an arrester hook (also from the spares box), and a pair of splayed stabilizer fins was added as a compensation. Finally, some of the OOB air scoops were placed all round the hull and some pitots, antennae and a gun camera fairing added.
Painting and markings:
This whif was to look naval at first sight, so I referred to the early Yak-38 VTOL aircraft and their rather minimalistic paint scheme in an overall dull blue. The green underside, seen on many service aircraft, was AFAIK a (later) protective coating – an obsolete detail for a CTOL aircraft.
Hence, all upper surfaces and the fuselage were painted in a uniform “Field Blue” (Tamiya XF-50). It’s a bit dark, but I have used this unique, petrol blue tone many moons ago on a real world Kangnam Forger where it looks pretty good, and in this case the surface was furthermore shaded with Humbrol 96 and 126 after a black in wash.
For some contrast I painted the undersides of the wings and stabilizers as well as a fuselage section between the wings in a pale grey (Humbrol 167), seen on one of the Yak-38 prototypes. Not very obvious, but at least the aircraft did not end up in a boring, uniform color.
The interior was painted in blue-gray (PRU Blue, shaded with Humbrol 87) while the landing gear wells became Aluminum (Humbrol 56). The wheel discs became bright green, just in order to keep in style and as a colorful contrast, and some di-electric panels and covers became very light grey or bright green. For some color contrast, the anti-flutter weight tips on the stabilizers as well as the pylons’ front ends were painted bright red.
The markings/decals reflect the early Soviet Navy style, with simple Red Stars, large yellow tactical codes and some high contrast warning stencils, taken from the remains of a Yak-38 sheet (American Revell re-release of the Kangnam kit).
Finally, after some soot stains with graphite around the gun muzzles and the air bleed doors, the kit was sealed with a coat of semi-matt acrylic varnish and some matt accents (anti-glare panel, radomes).
A simple idea that turned out to be more complex than expected, due to the wing fence troubles. But I am happy that the Attacker nose could be so easily transplanted, it changes the MiG-19’s look considerably, as well as the wings with (much) less sweep angle.
The aircraft looks familiar, but you only recognize at second glance that it is more than just a MiG-19 with a solid nose. The thing looks pretty retro, reminds me a bit of the Supermarine Scimitar (dunno?), and IMHO it appears more Chinese than Soviet (maybe because the layout reminds a lot of the Q-5 fighter bomber)? It could even, with appropriate markings, be a Luft ’46 design?
You may view more of my images of Ickworth House, Park and gardens, by clicking "here" !
With over 1,800 acres of parkland designed by Capability Brown, the house and its grounds were created as an homage to Italy, the country so beloved by Frederick Augustus Hervey, the 4th Earl of Bristol. The Earl-Bishop spent his life travelling the continent, gathering together a vast collection of paintings, sculpture and artefacts. Already possessed of several houses, he conceived Ickworth primarily as a museum for his treasures. At his death only the Rotunda - the giant circular structure at the centre of the two wings, described by Hervey's wife as 'a stupendous moment of Folly' - was nearing completion. The house was eventually finished by his son. Although Hervey's treasures, confiscated during the French invasion of Italy, were destined never to occupy Ickworth, his descendants made it their life's work to rebuild what has become an exceptional collection of art and silver. Paintings housed in the galleries include works by Velázquez, Titian and Poussin, while the collection of 18th-century portraits of the family is exceptionally fine, featuring canvases by Gainsborough, Reynolds, Vigée-Lebrun and Hogarth. In addition to one of the very best British collections of Georgian Huguenot silver, Ickworth is also home to an impressive array of Regency furniture, porcelain, and domestic objects. More made a career of producing idealised Italian landscapes. His Landscape with Classical Figures, Cicero at his Villa, painted in 1780 and funded in 1993, is a typical work, the misty soft-focus and pastel light adding to its appeal. Hugh Douglas Hamilton's The Earl Bishop of Bristol and Derry Seated before the Prospect of Rome shows Hervey seated at what is thought to be the southern tip of the Borghese Gardens. Ickworth's parklands and gardens can provide a day's activity in their own right. The south gardens are modelled on the formal Italian style, while the gardens to the west of the house are more informal. Visitors can walk or cycle out into the park itself and up to the Fairy Lake. Bright and modern, The West Wing Restaurant overlooks the gardens and can be guaranteed to catch any sunlight on offer. It serves everything from hot meals to snacks, and at weekends the restaurant is open for breakfast. If you're after something rather more formal, try Frederick's restaurant at Ickworth Hotel in the grounds.
A three-stage Soyuz is transferred by rail in a horizontal position from the MIK assembly facility to the launch zone at Europe's Spaceport in Kourou, French Guiana, in preparation for the launch of the first two ‘Full Operational Capability’ Galileo satellites. The satellites are set for liftoff on 22 August, at 12:27 UTC/14:27 CEST.
Read more about launching Galileo:
www.esa.int/Our_Activities/Navigation/The_future_-_Galile...
Credit: ESA-CNES-ARIANESPACE/Optique Vidéo du CSG - P.Baudon
TOPJACK is a modular Jack Up barge with 250 tonne lift
capability complete with 36m legs. Capable for supporting a wide
range of disciplines including port construction, safe investigation
and piling operations.
Ravestein Container Pontoon B.V.
TYPE RCP-250 – MODULAR SELF ELEVATING PLATFORM
Specification Jacking System
Type : Hydraulic cylinders
Jacking Capacity (4x) : 250 Ton at 250 bar
Locking : By means of hydraulic activated rotating locks Hydraulic Power Unit
Type : Electric Hydraulic driven powerpack
Controls : Remote control (incl. second cable control box)
Capacity HPU : 2x 55 kW
Location : In deck container, with small store Generator
Type : Silenced packed Caterpillar or equal, self supporting
Capacity : 220 kVa - On top of deck Container Classification:
German Lloyds : GL 100A5 K(20) Self Elevating Unit, Coastal Water (or equal)
Options (not included)
Positioning winches / Deck Crane / RCP Boarding System
Swim end units / Spud Cans
Additional Tanks and piping systems
Backhoe Configuration
Contact
David Ravestein / Aernout Goedbloed
Ravestein Container Pontoon B.V.
Waalbandijk 26; 6669 MB Dodewaard (Holland)
Tel +31 (0)488 - 41 18 01
Fax +31 (0)488 - 41 26 47
E-mail info@rcpbv.com
Website www.rcpbv.com
Local Notice to Mariners
Number: 10/25. Date: 13th May 2025
Exmouth Outfall - Marine Operations - ABCO Divers
Notice is hereby given that ABCO Divers intend to commence work on the Exmouth Outfall Diffuser Pit Excavations and Install on the earliest date of 17th May 2025 on behalf of South West Water Ltd. The works are programmed to be completed by July 2025.
Jack Up Barge “Top Jack 1” in Teignmouth Port, will be towed from Teignmouth as early as Saturday to the outfall site to the east of Exmouth, which is off Straight Point.
Position:
50°36'14.43" N
003°21'30.90" W
The support vessels “Jenny D” and “Celtic Avenger” will be assisting the project throughout the operation. Works will involve excavations from the Jack Up Barge, diving activities and lifting operations to support the install of the outfall diffusers.
All marine users are asked to observe a 500m exclusion zone around the Jack Up Barge.
Vessels
“Topjack 1” – 250t Jack Up Barge – 17m x 24m
“Jenny D” – 21.6m LOA, 9.04m Beam – Multicat and Tug Vessel - IMO 9570905, MMSI 235075339
“Celtic Avenger” – 14m Crew Transfer and Survey Vessel – MMSI 232055392
Pasted from Wikipedia: Bell-Boeing V-22 Osprey
• • • • •
The Bell-Boeing V-22 Osprey is a multi-mission, military, tiltrotor aircraft with both a vertical takeoff and landing (VTOL), and short takeoff and landing (STOL) capability. It is designed to combine the functionality of a conventional helicopter with the long-range, high-speed cruise performance of a turboprop aircraft.
The V-22 originated from the U.S. Department of Defense Joint-service Vertical take-off/landing Experimental (JVX) aircraft program started in 1981. It was developed jointly by the Bell Helicopter, and Boeing Helicopters team, known as Bell Boeing, which produce the aircraft.[4] The V-22 first flew in 1989, and began years of flight testing and design alterations.
The United States Marine Corps began crew training for the Osprey in 2000, and fielded it in 2007. The Osprey's other operator, the U.S. Air Force fielded their version of the tiltrotor in 2009. Since entering service with the U.S. Marine Corps and Air Force, the Osprey has been deployed for combat operations in Iraq and Afghanistan.
Contents
•• 1.2 Flight testing and design changes
• 2 Design
• 8 Notable appearances in media
Development
Early development
The failure of the Iran hostage rescue mission in 1980 demonstrated to the United States military a need[5] for "a new type of aircraft, that could not only take off and land vertically but also could carry combat troops, and do so at speed."[6] The U.S. Department of Defense began the Joint-service Vertical take-off/landing Experimental (JVX) aircraft program in 1981, under U.S. Army leadership. Later the U.S. Navy/Marine Corps took the lead.[7][8] The JVX combined requirements from the Marine Corps, Air Force, Army and Navy.[9][10] A request for proposals (RFP) was issued in December 1982 for JVX preliminary design work. Interest in the program was expressed by Aérospatiale, Bell Helicopter, Boeing Vertol, Grumman, Lockheed, and Westland. The DoD pushed for contractors to form teams. Bell partnered with Boeing Vertol. The Bell Boeing team submitted a proposal for a enlarged version of the Bell XV-15 prototype on 17 February 1983. This was the only proposal received and a preliminary design contract was awarded on 26 April 1983.[11][12]
The JVX aircraft was designated V-22 Osprey on 15 January 1985; by March that same year the first six prototypes were being produced, and Boeing Vertol was expanded to deal with the project workload.[13][14] Work has been split evenly between Bell and Boeing. Bell Helicopter manufactures and integrates the wing, nacelles, rotors, drive system, tail surfaces, and aft ramp, as well as integrates the Rolls-Royce engines and performs final assembly. Boeing Helicopters manufactures and integrates the fuselage, cockpit, avionics, and flight controls.[4][15] The USMC variant of the Osprey received the MV-22 designation and the Air Force variant received CV-22; reversed from normal procedure to prevent Marine Ospreys from having a conflicting designation with aircraft carriers (CV).[16] Full-scale development of the V-22 tilt-rotor aircraft began in 1986.[2] On 3 May 1986 the Bell-Boeing partnership was awarded a $1.714 billion contract for V-22 aircraft by the Navy, thus at this point the project had acquisition plans with all four arms of the U.S. military.[17]
The first V-22 was rolled out with significant media attention in May 1988.[18][19] However the project suffered several political blows. Firstly in the same year, the Army left the program, citing a need to focus its budget on more immediate aviation programs.[20] The project also faced considerable dialogue in the Senate, surviving two votes that both could have resulted in cancellation.[21][22] Despite the Senate's decision, the Department of Defense instructed the Navy not to spend more money on the Osprey.[23] At the same time, the Bush administration sought the cancellation of the project.[23]
Flight testing and design changes
The first of six MV-22 prototypes first flew on 19 March 1989 in the helicopter mode,[24] and on 14 September 1989 as a fixed-wing plane.[25] The third and fourth prototypes successfully completed the Osprey's first Sea Trials on the USS Wasp in December 1990.[26] However, the fourth and fifth prototypes crashed in 1991-92.[27] Flight tests were resumed in August 1993 after changes were incorporated in the prototypes.[2] From October 1992 until April 1993, Bell and Boeing redesigned the V-22 to reduce empty weight, simplify manufacture and reduce production costs. This redesigned version became the B-model.[28]
Flight testing of four full-scale development V-22s began in early 1997 when the first pre-production V-22 was delivered to the Naval Air Warfare Test Center, Naval Air Station Patuxent River, Maryland. The first EMD flight took place on 5 February 1997. The first of four low rate initial production aircraft, ordered on 28 April 1997, was delivered on 27 May 1999. Osprey number 10 completed the program's second Sea Trials, this time from the USS Saipan in January 1999.[2] During external load testing in April 1999, Boeing used a V-22 to lift and transport the M777 howitzer.[29] In 2000, Boeing announced that the V-22 would be fitted with a nose-mounted GAU-19 Gatling gun,[30] but the GAU-19 gun was later canceled.[31]
In 2000, there were two further fatal crashes, killing a total of 19 Marines, and the production was again halted while the cause of these crashes was investigated and various parts were redesigned.[32] The V-22 completed its final operational evaluation in June 2005. The evaluation was deemed successful; events included long range deployments, high altitude, desert and shipboard operations. The problems identified in various accidents had been addressed.[33]
Controversy
The V-22's development process has been long and controversial, partly due to its large cost increases.[34] When the development budget, first planned for $2.5 billion in 1986, increased to a projected $30 billion in 1988, then-Defense Secretary Dick Cheney tried to zero out its funding. He was eventually overruled by Congress.[32] As of 2008, $27 billion have been spent on the Osprey program and another $27.2 billion will be required to complete planned production numbers by the end of the program.[2]
The V-22 squadron's former commander at Marine Corps Air Station New River, Lt. Colonel Odin Lieberman, was relieved of duty in 2001 after allegations that he instructed his unit that they needed to falsify maintenance records to make the plane appear more reliable.[2][35] Three officers were later implicated in the falsification scandal.[34]
The aircraft is incapable of autorotation, and is therefore unable to land safely in helicopter mode if both engines fail. A director of the Pentagon's testing office in 2005 said that if the Osprey loses power while flying like a helicopter below 1,600 feet (490 m), emergency landings "are not likely to be survivable". But Captain Justin (Moon) McKinney, a V-22 pilot, says that this will not be a problem, "We can turn it into a plane and glide it down, just like a C-130".[31] A complete loss of power would require the failure of both engines, as a drive shaft connects the nacelles through the wing; one engine can power both proprotors.[36] While vortex ring state (VRS) contributed to a deadly V-22 accident, the aircraft is less susceptible to the condition than conventional helicopters and recovers more quickly.[5] The Marines now train new pilots in the recognition of and recovery from VRS and have instituted operational envelope limits and instrumentation to help pilots avoid VRS conditions.[32][37]
It was planned in 2000 to equip all V-22s with a nose-mounted Gatling gun, to provide "the V-22 with a strong defensive firepower capability to greatly increase the aircraft's survivability in hostile actions."[30] The nose gun project was canceled however, leading to criticism by retired Marine Corps Commandant General James L. Jones, who is not satisfied with the current V-22 armament.[31] A belly-mounted turret was later installed on some of the first V-22s sent to the War in Afghanistan in 2009.[38]
With the first combat deployment of the MV-22 in October 2007, Time Magazine ran an article condemning the aircraft as unsafe, overpriced, and completely inadequate.[31] The Marine Corps, however, responded with the assertion that much of the article's data were dated, obsolete, inaccurate, and reflected expectations that ran too high for any new field of aircraft.[39]
Recent development
On 28 September 2005, the Pentagon formally approved full-rate production for the V-22.[40] The plan is to boost production from 11 a year to between 24 and 48 a year by 2012. Of the 458 total planned, 360 are for the Marine Corps, 48 for the Navy, and 50 for the Air Force at an average cost of $110 million per aircraft, including development costs.[2] The V-22 had an incremental flyaway cost of $70 million per aircraft in 2007,[3] but the Navy hopes to shave about $10 million off that cost after a five-year production contract starts in 2008.[41]
The Bell-Boeing Joint Project Office in Amarillo, Texas will design a new integrated avionics processor to resolve electronics obsolescence issues and add new network capabilities.[42]
Design
The Osprey is the world's first production tiltrotor aircraft, with one three-bladed proprotor, turboprop engine, and transmission nacelle mounted on each wingtip. It is classified as a powered lift aircraft by the Federal Aviation Administration.[43] For takeoff and landing, it typically operates as a helicopter with the nacelles vertical (rotors horizontal). Once airborne, the nacelles rotate forward 90° in as little as 12 seconds for horizontal flight, converting the V-22 to a more fuel-efficient, higher-speed turboprop airplane. STOL rolling-takeoff and landing capability is achieved by having the nacelles tilted forward up to 45°. For compact storage and transport, the V-22's wing rotates to align, front-to-back, with the fuselage. The proprotors can also fold in a sequence taking 90 seconds.[44]
Most Osprey missions will use fixed wing flight 75 percent or more of the time, reducing wear and tear on the aircraft and reducing operational costs.[45] This fixed wing flight is higher than typical helicopter missions allowing longer range line-of-sight communications and so improved command and control.[2] Boeing has stated the V-22 design loses 10% of its vertical lift over a Tiltwing design when operating in helicopter mode because of airflow resistance due to the wings, but that the Tiltrotor design has better short takeoff and landing performance.[46]
The V-22 is equipped with a glass cockpit, which incorporates four Multi-function displays (MFDs) and one shared Central Display Unit (CDU), allowing the pilots to display a variety of images including: digimaps centered or decentered on current position, FLIR imagery, primary flight instruments, navigation (TACAN, VOR, ILS, GPS, INS), and system status. The flight director panel of the Cockpit Management System (CMS) allows for fully-coupled (aka: autopilot) functions which will take the aircraft from forward flight into a 50-foot hover with no pilot interaction other than programming the system.[47] The glass cockpit of the canceled CH-46X was derived from the V-22.[48]
The V-22 is a fly-by-wire aircraft with triple-redundant flight control systems.[49] With the nacelles pointing straight up in conversion mode at 90° the flight computers command the aircraft to fly like a helicopter, with cyclic forces being applied to a conventional swashplate at the rotor hub. With the nacelles in airplane mode (0°) the flaperons, rudder, and elevator fly the aircraft like an airplane. This is a gradual transition and occurs over the rotation range of the nacelles. The lower the nacelles, the greater effect of the airplane-mode control surfaces.[50] The nacelles can rotate past vertical to 97.5° for rearward flight.[51][52]
The Osprey can be armed with one M240 7.62x51mm NATO (.308 in caliber) or M2 .50 in caliber (12.7 mm) machine gun on the loading ramp, that can be fired rearward when the ramp is lowered. A GAU-19 three-barrel .50 in gatling gun mounted below the V-22's nose has also been studied for future upgrade.[31][53] BAE Systems developed a remotely operated turreted weapons system for the V-22,[54] which was installed on half of the first V-22s deployed to Afghanistan in 2009.[38] The 7.62 mm belly gun turret is remotely operated by a gunner inside the aircraft, who acquires targets with a separate pod using color television and forward looking infrared imagery.
U.S. Naval Air Systems Command is working on upgrades to increase the maximum speed from 250 knots (460 km/h; 290 mph) to 270 knots (500 km/h; 310 mph), increase helicopter mode altitude limit from 10,000 feet (3,000 m) to 12,000 feet (3,700 m) or 14,000 feet (4,300 m), and increase lift performance.[55]
Operational history
US Marine Corps
Marine Corps crew training on the Osprey has been conducted by VMMT-204 since March 2000. On 3 June 2005, the Marine Corps helicopter squadron Marine Medium Helicopter 263 (HMM-263), stood down to begin the process of transitioning to the MV-22 Osprey.[56] On 8 December 2005, Lieutenant General Amos, commander of the II MEF, accepted the delivery of the first fleet of MV-22s, delivered to HMM-263. The unit reactivated on 3 March 2006 as the first MV-22 squadron and was redesignated VMM-263. On 31 August 2006, VMM-162 (the former HMM-162) followed suit. On 23 March 2007, HMM-266 became Marine Medium Tiltrotor Squadron 266 (VMM-266) at Marine Corps Air Station New River, North Carolina.[57]
The Osprey has been replacing existing CH-46 Sea Knight squadrons.[58] The MV-22 reached initial operational capability (IOC) with the U.S. Marine Corps on 13 June 2007.[1] On 10 July 2007 an MV-22 Osprey landed aboard the Royal Navy aircraft carrier, HMS Illustrious in the Atlantic Ocean. This marked the first time a V-22 had landed on any non-U.S. vessel.[59]
On 13 April 2007, the U.S. Marine Corps announced that it would be sending ten V-22 aircraft to Iraq, the Osprey's first combat deployment. Marine Corps Commandant, General James Conway, indicated that over 150 Marines would accompany the Osprey set for September deployment to Al-Asad Airfield.[60][61] On 17 September 2007, ten MV-22Bs of VMM-263 left for Iraq aboard the USS Wasp. The decision to use a ship rather than use the Osprey's self-deployment capability was made because of concerns over icing during the North Atlantic portion of the trip, lack of available KC-130s for mid-air refueling, and the availability of the USS Wasp.[62]
The Osprey has provided support in Iraq, racking up some 2,000 flight hours over three months with a mission capable availability rate of 68.1% as of late-January 2008.[63] They are primarily used in Iraq's western Anbar province for routine cargo and troop movements, and also for riskier "aero-scout" missions. General David Petraeus, the top U.S. military commander in Iraq, used one to fly around Iraq on Christmas Day 2007 to visit troops.[64] Then-presidential candidate Barack Obama also flew in Ospreys during his high profile 2008 tour of Iraq.[65]
The only major problem has been obtaining the necessary spare parts to maintain the aircraft.[66] The V-22 had flown 3,000 sorties totaling 5,200 hours in Iraq as of July 2008.[67] USMC leadership expect to deploy MV-22s to Afghanistan in 2009.[66][68] General George J. Trautman, III praised the increased range of the V-22 over the legacy helicopters in Iraq and said that "it turned his battle space from the size of Texas into the size of Rhode Island."[69]
Naval Air Systems Command has devised a temporary fix for sailors to place portable heat shields under Osprey engines to prevent damage to the decks of some of the Navy's smaller amphibious ships, but they determined that a long term solution to the problem would require these decks be redesigned with heat resistant deck coatings, passive thermal barriers and changes in ship structure in order to operate V-22s and F-35Bs.[70]
A Government Accountability Office study reported that by January 2009 the Marines had 12 MV-22s operating in Iraq and they managed to successfully complete all assigned missions. The same report found that the V-22 deployments had mission capable rates averaging 57% to 68% and an overall full mission capable rate of only 6%. It also stated that the aircraft had shown weakness in situational awareness, maintenance, shipboard operations and the ability to transport troops and external cargo.[71] That study also concluded that the "deployments confirmed that the V-22’s enhanced speed and range enable personnel and internal cargo to be transported faster and farther than is possible with the legacy helicopters it is replacing".[71]
The MV-22 saw its first offensive combat mission, Operation Cobra's Anger on 4 December 2009. Ospreys assisted in inserting 1,000 Marines and 150 Afghan troops into the Now Zad Valley of Helmand Province in southern Afghanistan to disrupt communication and supply lines of the Taliban.[38] In January 2010 the MV-22 Osprey is being sent to Haiti as part of Operation Unified Response relief efforts after the earthquake there. This will be the first use the Marine V-22 in a humanitarian mission.[72]
US Air Force
The Air Force's first operational CV-22 Osprey was delivered to the 58th Special Operations Wing (58th SOW) at Kirtland Air Force Base, New Mexico on 20 March 2006. This and subsequent aircraft will become part of the 58th SOW's fleet of aircraft used for training pilots and crew members for special operations use.[73] On 16 November 2006, the Air Force officially accepted the CV-22 in a ceremony conducted at Hurlburt Field, Florida.[74]
The US Air Force's first operational deployment of the Osprey sent four CV-22s to Mali in November 2008 in support of Exercise Flintlock. The CV-22s flew nonstop from Hurlburt Field, Florida with in-flight refueling.[5] AFSOC declared that the 8th Special Operations Squadron reached Initial Operational Capability on 16 March 2009, with six of its planned nine CV-22s operational.[75]
In June 2009, CV-22s of the 8th Special Operations Squadron delivered 43,000 pounds (20,000 kg) of humanitarian supplies to remote villages in Honduras that were not accessible by conventional vehicles.[76] In November 2009, the 8th SO Squadron and its six CV-22s returned from a three-month deployment in Iraq.[77]
The first possible combat loss of an Osprey occurred on 9 April, 2010, as a CV-22 went down near Qalat, Zabul Province, Afghanistan, killing four.[78][79]
Potential operators
In 1999 the V-22 was studied for use in the United Kingdom's Royal Navy,[80] it has been raised several times as a candidate for the role of Maritime Airborne Surveillance and Control (MASC).[81]
Israel had shown interest in the purchase of MV-22s, but no order was placed.[82][83] Flightglobal reported in late 2009 that Israel has decided to wait for the CH-53K instead.[84]
The V-22 Osprey is a candidate for the Norwegian All Weather Search and Rescue Helicopter (NAWSARH) that is planned to replace the Westland Sea King Mk.43B of the Royal Norwegian Air Force in 2015.[85] The other candidates for the NAWSARH contract of 10-12 helicopters are AgustaWestland AW101 Merlin, Eurocopter EC225, NHIndustries NH90 and Sikorsky S-92.[86]
Bell Boeing has made an unsolicited offer of the V-22 for US Army medical evacuation needs.[87] However the Joint Personnel Recovery Agency issued a report that said that a common helicopter design would be needed for both combat recovery and medical evacuation and that the V-22 would not be suitable for recovery missions because of the difficulty of hoist operations and lack of self-defense capabilities.[88]
The US Navy remains a potential user of the V-22, but its role and mission with the Navy remains unclear. The latest proposal is to replace the C-2 Greyhound with the V-22 in the fleet logistics role. The V-22 would have the advantage of being able to land on and support non-carriers with rapid delivery of supplies and people between the ships of a taskforce or to ships on patrol beyond helicopter range.[89] Loren B. Thompson of the Lexington Institute has suggested V-22s for use in combat search and rescue and Marine One VIP transport, which also need replacement aircraft.[90]
Variants
• V-22A
•• Pre-production full-scale development aircraft used for flight testing. These are unofficially considered A-variants after 1993 redesign.[91]
• HV-22
•• The U.S. Navy considered an HV-22 to provide combat search and rescue, delivery and retrieval of special warfare teams along with fleet logistic support transport. However, it chose the MH-60S for this role in 1992.[92]
• SV-22
•• The proposed anti-submarine warfare Navy variant. The Navy studied the SV-22 in the 1980s to replace S-3 and SH-2 aircraft.[93]
• MV-22B
•• Basic U.S. Marine Corps transport; original requirement for 552 (now 360). The Marine Corps is the lead service in the development of the V-22 Osprey. The Marine Corps variant, the MV-22B, is an assault transport for troops, equipment and supplies, capable of operating from ships or from expeditionary airfields ashore. It is replacing the Marine Corps' CH-46E[57] and CH-53D.[94]
• CV-22B
•• Air Force variant for the U.S. Special Operations Command (USSOCOM). It will conduct long-range, special operations missions, and is equipped with extra fuel tanks and terrain-following radar.[95][96]
Operators
•• 8th Special Operations Squadron (8 SOS) at Hurlburt Field, Florida
•• 71st Special Operations Squadron (71 SOS) at Kirtland Air Force Base, New Mexico
•• 20th Special Operations Squadron (20 SOS) at Cannon Air Force Base, New Mexico
•• VMM-161
•• VMM-162
•• VMM-261
•• VMM-263
•• VMM-264
•• VMM-266
•• VMM-365
•• VMMT-204 - Training squadron
•• VMX-22 - Marine Tiltrotor Operational Test and Evaluation Squadron
Notable accidents
Main article: Accidents and incidents involving the V-22 Osprey
From 1991 to 2000 there were four significant crashes, and a total of 30 fatalities, during testing.[32] Since becoming operational in 2007, the V-22 has had one possible combat loss due to an unknown cause, no losses due to accidents, and seven other notable, but minor, incidents.
• On 11 June 1991, a mis-wired flight control system led to two minor injuries when the left nacelle struck the ground while the aircraft was hovering 15 feet (4.6 m) in the air, causing it to bounce and catch fire.[97]
• On 20 July 1992, a leaking gearbox led to a fire in the right nacelle, causing the aircraft to drop into the Potomac River in front of an audience of Congressmen and other government officials at Quantico, killing all seven on board and grounding the aircraft for 11 months.[98]
• On 8 April 2000, a V-22 loaded with Marines to simulate a rescue, attempted to land at Marana Northwest Regional Airport in Arizona, stalled when its right rotor entered vortex ring state, rolled over, crashed, and exploded, killing all 19 on board.[37]
• On 11 December 2000, after a catastrophic hydraulic leak and subsequent software instrument failure, a V-22 fell 1,600 feet (490 m) into a forest in Jacksonville, North Carolina, killing all four aboard. This caused the Marine Corps to ground their fleet of eight V-22s, the second grounding that year.[99][100]
Specifications (MV-22B)
Data from Boeing Integrated Defense Systems,[101] Naval Air Systems Command,[102] US Air Force CV-22 fact sheet,[95] Norton,[103] and Bell[104]
General characteristics
• Crew: Four (pilot, copilot and two flight engineers)
• Capacity: 24 troops (seated), 32 troops (floor loaded) or up to 15,000 lb (6,800 kg) of cargo (dual hook)
• Length: 57 ft 4 in (17.5 m)
• Rotor diameter: 38 ft 0 in (11.6 m)
• Wingspan: 45 ft 10 in (14 m)
• Width with rotors: 84 ft 7 in (25.8 m)
• Height: 22 ft 1 in/6.73 m; overall with nacelles vertical (17 ft 11 in/5.5 m; at top of tailfins)
• Disc area: 2,268 ft² (212 m²)
• Wing area: 301.4 ft² (28 m²)
• Empty weight: 33,140 lb (15,032 kg)
• Loaded weight: 47,500 lb (21,500 kg)
• Max takeoff weight: 60,500 lb (27,400 kg)
• Powerplant: 2× Rolls-Royce Allison T406/AE 1107C-Liberty turboshafts, 6,150 hp (4,590 kW) each
Performance
• Maximum speed: 250 knots (460 km/h, 290 mph) at sea level / 305 kn (565 km/h; 351 mph) at 15,000 ft (4,600 m)[105]
• Cruise speed: 241 knots (277 mph, 446 km/h) at sea level
• Range: 879 nmi (1,011 mi, 1,627 km)
• Combat radius: 370 nmi (426 mi, 685 km)
• Ferry range: 1,940 nmi (with auxiliary internal fuel tanks)
• Service ceiling: 26,000 ft (7,925 m)
• Rate of climb: 2,320 ft/min (11.8 m/s)
• Disc loading: 20.9 lb/ft² at 47,500 lb GW (102.23 kg/m²)
• Power/mass: 0.259 hp/lb (427 W/kg)
Armament
• 1× M240 machine gun on ramp, optional
Notable appearances in media
Main article: Aircraft in fiction#V-22 Osprey
See also
• Elizabeth A. Okoreeh-Baah, USMC - first female to pilot a V-22 Osprey
Related development
Comparable aircraft
Related lists
• List of military aircraft of the United States
References
Bibliography
• Markman, Steve and Bill Holder. "Bell/Boeing V-22 Osprey Tilt-Engine VTOL Transport (U.S.A.)". Straight Up: A History of Vertical Flight. Schiffer Publishing, 2000. ISBN 0-7643-1204-9.
• Norton, Bill. Bell Boeing V-22 Osprey, Tiltrotor Tactical Transport. Midland Publishing, 2004. ISBN 1-85780-165-2.
External links
Wikimedia Commons has media related to: V-22 Osprey
• V-22 Osprey web, and www.history.navy.mil/planes/v-22.html
• CV-22 fact sheet on USAF site
• www.globalsecurity.org/military/systems/aircraft/v-22.htm
• www.airforce-technology.com/projects/osprey/
• "Flight of the Osprey", US Navy video of V-22 operations
To the west of Bath looking towards the village of Corston to the left and Saltford in the centre. Kelston Park dominates the hill to the right and is a Grade II* listed building which at the time of the photograph was used as offices. The original house was built between 1765 and 1770, the architect being John Wood the Younger, for Sir Caesar Hawkins who was Serjeant-Surgeon to King George II and King George III. Sir Caesar commissioned Capability Brown to lay out the park, which is also Grade II* listed, in 1767-68.
The Citroën 2CV (French: "deux chevaux" i.e. "deux chevaux-vapeur" (lit. "two steam horses", "two tax horsepower") is an air-cooled front-engine, front-wheel-drive economy car introduced at the 1948 Paris Mondial de l'Automobile and manufactured by Citroën for model years 1948–1990.
Conceived by Citroën Vice-President Pierre Boulanger to help motorise the large number of farmers still using horses and carts in 1930s France, the 2CV has a combination of innovative engineering and utilitarian, straightforward metal bodywork — initially corrugated for added strength without added weight. The 2CV featured low cost; simplicity of overall maintenance; an easily serviced air-cooled engine (originally offering 9 hp); low fuel consumption; and an extremely long-travel suspension offering a soft ride and light off-road capability. Often called "an umbrella on wheels", the fixed-profile convertible bodywork featured a full-width, canvas, roll-back sunroof, which accommodated oversized loads and until 1955 reached almost to the car's rear bumper.
Manufactured in France between 1948 and 1989 (and in Portugal from 1989 to 1990), over 3.8 million 2CVs were produced, along with over 1.2 million small 2CV-based delivery vans known as Fourgonnettes. Citroën ultimately offered several mechanically identical variants including the Ami (over 1.8 million); the Dyane (over 1.4 million); the Acadiane (over 250,000); and the Mehari (over 140,000). In total, Citroën manufactured almost 7 million 2CV variants.
A 1953 technical review in Autocar described "the extraordinary ingenuity of this design, which is undoubtedly the most original since the Model T Ford". In 2011, The Globe and Mail called it a "car like no other". The motoring writer L. J. K. Setright described the 2CV as "the most intelligent application of minimalism ever to succeed as a car", and a car of "remorseless rationality".]
HISTORY
DEVELOPMENT
In 1934, family-owned Michelin, being the largest creditor, took over the bankrupt Citroën company. The new management ordered a new market survey, conducted by Jacques Duclos. France at that time had a large rural population which could not yet afford cars; Citroën used the survey results to prepare a design brief for a low-priced, rugged "umbrella on four wheels" that would enable four people to transport 50 kg of farm goods to market at 50 km/h, if necessary across muddy, unpaved roads. In fuel economy, the car would use no more than 3 l/100 km (95 mpg-imp). One design requirement was that the customer be able to drive eggs across a freshly ploughed field without breaking them.
In 1936, Pierre-Jules Boulanger, vice-president of Citroën and chief of engineering and design, sent the brief to his design team at the engineering department. The TPV (Toute Petite Voiture — "Very Small Car") was to be developed in secrecy at Michelin facilities at Clermont-Ferrand and at Citroën in Paris, by the design team who had created the Traction Avant.
Boulanger was closely involved with all decisions relating to the TPV, and was determined to reduce the weight to targets that his engineers thought impossible. He set up a department to weigh every component and then redesign it, to make it lighter while still doing its job.
Boulanger placed engineer André Lefèbvre in charge of the TPV project. Lefèbvre had designed and raced Grand Prix cars; his speciality was chassis design and he was particularly interested in maintaining contact between tyres and the road surface.
The first prototypes were bare chassis with rudimentary controls, seating and roof; test drivers wore leather flying suits, of the type used in contemporary open biplanes. By the end of 1937 20 TPV experimental prototypes had been built and tested. The prototypes had only one headlight, all that was required by French law at the time. At the end of 1937 Pierre Michelin was killed in a car crash; Boulanger became president of Citroën.
By 1939 the TPV was deemed ready, after 47 technically different and incrementally improved experimental prototypes had been built and tested. These prototypes used aluminium and magnesium parts and had water-cooled flat twin engines with front-wheel drive. The seats were hammocks hung from the roof by wires. The suspension system, designed by Alphonse Forceau, used front leading arms and rear trailing arms, connected to eight torsion bars beneath the rear seat: a bar for the front axle, one for the rear axle, an intermediate bar for each side, and an overload bar for each side. The front axle was connected to its torsion bars by cable. The overload bar came into play when the car had three people on board, two in the front and one in the rear, to support the extra load of a fourth passenger and fifty kilograms of luggage.
In mid-1939 a pilot run of 250 cars was produced and on 28 August 1939 the car received approval for the French market. Brochures were printed and preparations made to present the car, renamed the Citroën 2CV, at the forthcoming Paris Motor Show in October 1939.
WORLD WAR II
On 3 September 1939, France declared war on Germany following that country's invasion of Poland. An atmosphere of impending disaster led to the cancellation of the 1939 motor show less than a month before it was scheduled to open. The launch of the 2CV was abandoned.
During the German occupation of France in World War II Boulanger personally refused to collaborate with German authorities to the point where the Gestapo listed him as an "enemy of the Reich", under constant threat of arrest and deportation to Germany.
Michelin (Citroën's main shareholder) and Citroën managers decided to hide the TPV project from the Nazis, fearing some military application as in the case of the future Volkswagen Beetle, manufactured during the war as the military Kübelwagen. Several TPVs were buried at secret locations; one was disguised as a pickup, the others were destroyed, and Boulanger spent the next six years thinking about further improvements. Until 1994, when three TPVs were discovered in a barn, it was believed that only two prototypes had survived. As of 2003 there were five known TPVs.
By 1941, after an increase in aluminium prices of forty percent, an internal report at Citroën showed that producing the TPV post-war would not be economically viable, given the projected further increasing cost of aluminium. Boulanger decided to redesign the car to use mostly steel with flat panels, instead of aluminium. The Nazis had attempted to loot Citroën's press tools; this was frustrated after Boulanger got the French Resistance to re-label the rail cars containing them in the Paris marshalling yard. They ended up all over Europe, and Citroën was by no means sure they would all be returned after the war. In early 1944 Boulanger made the decision to abandon the water-cooled two-cylinder engine developed for the car and installed in the 1939 versions. Walter Becchia was now briefed to design an air-cooled unit, still of two cylinders, and still of 375 cc. Becchia was also supposed to design a three-speed gearbox, but managed to design a four-speed for the same space at little extra cost. At this time small French cars like the Renault Juvaquatre and Peugeot 202 usually featured three-speed transmissions, as did Citroën's own mid-size Traction Avant - but the 1936 Italian Fiat 500 "Topolino" "people's car" did have a four-speed gearbox. Becchia persuaded Boulanger that the fourth gear was an overdrive. The increased number of gear ratios also helped to pull the extra weight of changing from light alloys to steel for the body and chassis. Other changes included seats with tubular steel frames with rubber band springing and a restyling of the body by the Italian Flaminio Bertoni. Also, in 1944 the first studies of the Citroën hydro-pneumatic suspension were conducted using the TPV/2CV.
The development and production of what was to become the 2CV was also delayed by the incoming 1944 Socialist French government, after the liberation by the Allies from the Germans. The five-year "Plan Pons" to rationalise car production and husband scarce resources, named after economist and former French motor industry executive Paul-Marie Pons, only allowed Citroën the upper middle range of the car market, with the Traction Avant. The French government allocated the economy car market, US Marshall Plan aid, US production equipment and supplies of steel, to newly nationalised Renault to produce their Renault 4CV. The "Plan Pons" came to an end in 1949. Postwar French roads were very different from pre-war ones. Horse-drawn vehicles had re-appeared in large numbers. The few internal combustion-engined vehicles present often ran on town gas stored in gasbags on roofs or wood/charcoal gas from gasifiers on trailers. Only one hundred thousand of the two million pre-war cars were still on the road. The time was known as "Les années grises" or "the grey years" in France.
PRODUCTION
Citroën unveiled the car at the Paris Salon on 7 October 1948. The car on display was nearly identical to the 2CV type A that would be sold the next year, but it lacked an electric starter, the addition of which was decided the day before the opening of the Salon, replacing the pull cord starter. The canvas roof could be rolled completely open. The Type A had one stop light, and was only available in grey. The fuel level was checked with a dip stick/measuring rod, and the speedometer was attached to the windscreen pillar. The only other instrument was an ammeter.In 1949 the first delivered 2CV type A was 375 cc, 9 hp, with a 65 km/h top speed, only one tail light and windscreen wiper with speed shaft drive; the wiper speed was dependent on the driving speed. The car was heavily criticised by the motoring press and became the butt of French comedians for a short while. One American motoring journalist quipped, "Does it come with a can opener?" The British Autocar correspondent wrote that the 2CV "is the work of a designer who has kissed the lash of austerity with almost masochistic fervour".
Despite critics, Citroën was flooded with customer orders at the show. The car had a great impact on the lives of the low-income segment of the population in France. The 2CV was a commercial success: within months of it going on sale, there was a three-year waiting list, which soon increased to five years. At the time a second-hand 2CV was more expensive than a new one because the buyer did not have to wait. Production was increased from 876 units in 1949 to 6,196 units in 1950.
Grudging respect began to emanate from the international press: towards the end of 1951 the opinion appeared in Germany's recently launched Auto, Motor und Sport magazine that, despite its "ugliness and primitiveness" ("Häßlichkeit und Primitivität"), the 2CV was a "highly interesting" ("hochinteressantes") car.
In 1950, Pierre-Jules Boulanger was killed in a car crash on the main road from Clermont-Ferrand (the home of Michelin) to Paris.
In 1951 the 2CV received an ignition lock and a lockable driver's door. Production reached 100 cars a week. By the end of 1951 production totalled 16,288. Citroën introduced the 2CV Fourgonnette van. The "Weekend" version of the van had collapsible, removable rear seating and rear side windows, enabling a tradesman to use it as a family vehicle on the weekend as well as for business in the week.
By 1952, production had reached more than 21,000 with export markets earning foreign currency taking precedence. Boulanger's policy, which continued after his death, was: "Priority is given to those who have to travel by car because of their work, and for whom ordinary cars are too expensive to buy." Cars were sold preferentially to country vets, doctors, midwives, priests and small farmers. In 1954 the speedometer got a light for night driving. In 1955 the 2CV side repeaters were added above and behind the rear doors. It was now also available with 425 cc (AZ), 12.5 hp and a top speed of 80 km/h. In 1957 a heating and ventilation system was installed. The colour of the steering wheel changed from black to grey. The mirrors and the rear window were enlarged. The bonnet was decorated with a longitudinal strip of aluminium (AZL). In September 1957, the model AZLP (P for porte de malle, "boot lid"), appeared with a boot lid panel; previously the soft top had to be opened at the bottom to get to the boot. In 1958 a Belgian Citroën plant produced a higher quality version of the car (AZL3). It had a third side window, not available in the normal version, and improved details.
In 1960 the production of the 375 cc engine ended. The corrugated metal bonnet was replaced by a 5-rib glossy cover.
The 2 CV 4 × 4 2CV Sahara appeared in December 1960. This had an additional engine-transmission unit in the rear, mounted the other way around and driving the rear wheels. For the second engine there was a separate push-button starter and choke. With a gear stick between the front seats, both transmissions were operated simultaneously. For the two engines, there were separate petrol tanks under the front seats. The filler neck sat in the front doors. Both engines (and hence axles) could be operated independently. The spare wheel was mounted on the bonnet. 693 were produced until 1968 and one more in 1971. Many were used by the Swiss Post as a delivery vehicle. Today they are highly collectable.
From the mid-1950s economy car competition had increased — internationally in the form of the 1957 Fiat 500 and 1955 Fiat 600, and 1959 Austin Mini. By 1952, Germany produced a price-competitive car - the Messerschmitt KR175, followed in 1955 by the Isetta - these were microcars, not complete four-door cars like the 2CV. On the French home market, from 1961, the small Simca 1000 using licensed Fiat technology, and the larger Renault 4 hatchback had become available. The R4 was the biggest threat to the 2CV, eventually outselling it.
1960s
In 1960 the corrugated Citroën H Van style "ripple bonnet" of convex swages was replaced (except for the Sahara), with one using six larger concave swages and looked similar until the end of production. The 2CV had suicide doors in front from 1948 to 1964, replaced with front hinged doors from 1965 to 1990.
In 1961 Citroën launched a new model based on the 2CV chassis, with a 4-door sedan body, and a reverse rake rear window: the Citroën Ami. In 1962 the engine power was increased to 14 hp and top speed to 85 km/h. A sun roof was installed. In 1963 the engine power was increased to 16 hp. An electric wiper motor replaced the drive on the speedo. The ammeter was replaced by a charging indicator light. The speedometer was moved from the window frame into the dash. Instead of a dip stick/measuring rod, a fuel gauge was introduced.
Director of publicity Claude Puech came up with humorous and inventive marketing campaigns. Robert Delpire of the Delpire Agency was responsible for the brochures. Ad copy came from Jacques Wolgensinger Director of PR at Citroën. Wolgensinger was responsible for the youth orientated "Raids", 2CV Cross, rallies, the use of "Tin-Tin", and the slogan "More than just a car — a way of life". A range of colours was introduced, starting with Glacier Blue in 1959, then yellow in 1960. In the 1960s 2CV production caught up with demand. In 1966 the 2CV got a third side window. From September 1966 a Belgian-produced variant was sold in Germany with the 602 cc engine and 21 hp Ami6, the 3 CV (AZAM6). This version was only sold until 1968 in some export markets.
In 1967 Citroën launched a new model based on the 2CV chassis, with an updated but still utilitarian body, with a hatchback (a hatchback kit was available from Citroën dealers for the 2CV, and aftermarket kits are available) that boosted practicality: the Citroën Dyane. The exterior is more modern and distinguished by the recessed lights in the fenders and bodywork. Between 1967 and 1983 about 1.4 million were built. This was in response to competition by the Renault 4. The Dyane was originally planned as an upmarket version of the 2CV and was supposed to supersede it, but ultimately the 2CV outlived the Dyane by seven years. Citroën also developed the Méhari off-roader.
From 1961, the car was offered, at extra cost, with the flat-2 engine size increased to 602 cc, although for many years the smaller 425 cc engine continued to be available in France and export markets where engine size determined car tax levels. This was replaced by an updated 435 cc engine in 1968.
1970s
In 1970 the car gained rear light units from the Citroën Ami 6, and also standardised a third side window in the rear pillar on 2CV6 (602 cc) models. From 1970, only two series were produced: the 2CV 4 (AZKB) with 435 cc and the 2CV 6 (Azka) with 602 cc displacement. All 2CVs from this date can run on unleaded fuel. 1970s cars featured rectangular headlights, except the Spécial model. In 1971 the front bench seat was replaced with two individual seats. In 1972 2CVs were fitted with standard three-point seat belts. In 1973 new seat covers, a padded single-spoke steering wheel and ashtrays were introduced.
The highest annual production was in 1974. Sales of the 2CV were reinvigorated by the 1974 oil crisis. The 2CV after this time became as much a youth lifestyle statement as a basic functional form of transport. This renewed popularity was encouraged by the Citroën "Raid" intercontinental endurance rallies of the 1970s where customers could participate by buying a new 2CV, fitted with a "P.O." kit (Pays d'Outre-mer — overseas countries), to cope with thousands of miles of very poor or off-road routes.
1970: Paris–Kabul: 1,300 young people, 500 2CVs, 16,500 km to Afghanistan and back.
1971: Paris–Persepolis: 500 2CVs 13,500 km to Iran and back.
1973: Raid Afrique, 60 2CVs 8000 km from Abidjan to Tunis, the Atlantic capital of Ivory Coast through the Sahara, (the Ténéré desert section was unmapped and had previously been barred to cars), to the Mediterranean capital of Tunisia.
The Paris to Persepolis rally was the most famous. The Citroën "2CV Cross" circuit/off-road races were very popular in Europe.
Because of new emission standards, in 1975 power was reduced from 28 hp to 25 hp. The round headlights were replaced by square ones, adjustable in height. A new plastic grille was fitted.
In July 1975, a base model called the 2CV Spécial was introduced with the 435 cc engine. Between 1975 and 1990 under the name of AZKB "2CV Spécial" a drastically reduced trim basic version was sold, at first only in yellow. The small, square speedometer (which dates back to the Traction Avant), and the narrow rear bumper was installed. Citroën removed the third side window, the ashtray, and virtually all trim from the car. It also had the earlier round headlights. From the 1978 Paris Motor Show the Spécial regained third side windows, and was available in red and white; beginning in mid-1979 the 602 cc engine was installed. In June 1981 the Spécial E arrived; this model had a standard centrifugal clutch and particularly low urban fuel consumption.
1980s
In 1981 a yellow 2CV6 was driven by James Bond (Roger Moore) in the 1981 film For Your Eyes Only. The car in the film was fitted with the flat-4 engine from a Citroën GS which more than doubled the power. In one scene the ultra light 2CV tips over and is quickly righted by hand. Citroën launched a special edition 2CV "007" to coincide with the film; it was fitted with the standard engine and painted yellow with "007" on the front doors and fake bullet hole stickers.
In 1982 all 2CV models got inboard front disc brakes.
In 1988, production ended in France after 40 years but continued at the Mangualde plant in Portugal. This lasted until 1990, when production of the 2CV ended. The 2CV outlasted the Visa, another of the cars which might have been expected to replace it, and was produced for four years after the start of Citroën AX production.
Portuguese-built cars, especially those from when production was winding down, have a reputation in the UK for being much less well made and more prone to corrosion than those made in France. According to Citroën, the Portuguese plant was more up-to-date than the one in Levallois near Paris, and Portuguese 2CV manufacturing was to higher quality standards.
As of October 2016, 3,025 remained in service in the UK.
SPECIAL EDITION SALOON MODELS
The special edition models began with the 1976 SPOT model and continued in the with the 1980 Charleston, inspired by Art-Deco two colour styles 1920s Citroën model colour schemes. In 1981 the 007 arrived. In 1983 the 2CV Beachcomber arrived in the United Kingdom; it was known as "France 3" in France or "Transat" in other continental European markets — Citroën sponsored the French America's Cup yacht entry of that year. In 1985 the two-coloured Dolly appeared, using the "Spécial" model's basic trim rather than the slightly better-appointed "Club" as was the case with the other special editions. In 1986 there was the Cocorico. This means "cock-a-doodle-doo" and tied in with France's entry in the 1986 World Cup. "Le Coq Gaulois" or Gallic rooster is an unofficial national symbol of France. In 1987 came the Bamboo, followed by the 1988 Perrier in association with the mineral water company.
The Charleston, having been presented in October 1980 as a one-season "special edition" was incorporated into the regular range in July 1981 in response to its "extraordinary success". By changing the carburetor to achieve 29 hp a top speed of 115 km/h was achieved. Other changes were a new rear-view mirror and inboard disc brakes at the front wheels. In the 1980s there was a range of four full models:
Spécial
Dolly (an improved version of the Spécial)
Club (discontinued in the early 1980s)
Charleston (an improved version of the Club)
In Germany and Switzerland a special edition called, "I Fly Bleifrei" — "I Fly Lead Free" was launched in 1986, that could use unleaded, instead of then normal leaded petrol and super unleaded. It was introduced mainly because of stricter emissions standards. In 1987 it was replaced by the "Sausss-duck" special edition.
EXPORT MARKETS
The 2CV was originally sold in France and some European markets, and went on to enjoy strong sales in Asia, South America, and Africa. During the post-war years Citroën was very focused on the home market, which had some unusual quirks, like puissance fiscale. The management of Michelin was supportive of Citroën up to a point, and with a suspension designed to use Michelin's new radial tyres the Citroën cars clearly demonstrated their superiority over their competitors' tyres. But they were not prepared to initiate the investment needed for the 2CV (or the Citroën DS for that matter) to truly compete on the global stage. Citroën was always under-capitalised until the 1970s Peugeot takeover. The 2CV sold 8,830,679 vehicles; the Volkswagen Beetle, which was available worldwide, sold 21 million units.
CONSTRUCTION
The level of technology in the 1948 2CV was remarkable for the era. While colours and detail specifications were modified in the ensuing 42 years, the biggest mechanical change was the addition of front disc brakes (by then already fitted for several years in the mechanically similar Citroën Dyane 6), in October 1981 (for the 1982 model year). The reliability of the car was enhanced by the minimalist simplification of the designers, being air-cooled (with an oil cooler), it had no coolant, radiator, water pump or thermostat. It had no distributor either, just a contact breaker system. Except for the brakes, there were no hydraulic parts on original models; damping was by tuned mass dampers and friction dampers.
The 1948 car featured radial tyres, which had just been commercialised; front-wheel drive; rack and pinion steering mounted inside the front suspension cross-tube, away from a frontal impact; rear fender skirts (the suspension design allowed wheel changes without removing the skirts); bolt-on detachable front and rear wings; detachable doors, bonnet (and boot lid after 1960), by "slide out" P-profile sheet metal hinges; flap-up windows, as roll up windows were considered too heavy and expensive.; and detachable full length fabric sunroof and boot lid, for almost pickup-like load-carrying versatility. Ventilation in addition to the sunroof and front flap windows was provided by an opening flap under the windscreen. The car had load adjustable headlights and a heater (heaters were standardised on British economy cars in the 1960s).
BODY
The body was constructed of a dual H-frame platform chassis and aircraft-style tube framework, and a very thin steel shell that was bolted to the chassis. Because the original design brief called for a low speed car, little or no attention was paid to aerodynamics; the body had a drag coefficient of Cd=0.51, high by today's standards but typical for the era.
The 2CV used the fixed-profile convertible, where the doors and upper side elements of its bodywork remain fixed, while its fabric soft top can be opened. This reduces weight and lowers the centre of gravity, and allows the carrying of long or irregularly shaped items, but the key reason was that fabric was cheaper than steel which was in short supply and expensive after the war. The fixed-profile concept was quite popular in this period.
SUSPENSION
The suspension of the 2CV was very soft; a person could easily rock the car side to side dramatically. The swinging arm, fore-aft linked suspension system with inboard front brakes had a much smaller unsprung mass than existing coil spring or leaf spring designs. The design was modified by Marcel Chinon.
The system comprises two suspension cylinders mounted horizontally on each side of the platform chassis. Inside the cylinders are two springs, one for each wheel, mounted at each end of the cylinder. The springs are connected to the front leading swinging arm and rear trailing swinging arm, that act like bellcranks by pull rods (tie rods). These are connected to spring seating cups in the middle of the cylinder, each spring being compressed independently, against the ends of the cylinder. Each cylinder is mounted using an additional set of springs, originally made from steel, called "volute" springs, on later models made from rubber. These allow the front and rear suspension to interconnect. When the front wheel is deflected up over a bump, the front pull rod compresses the front spring inside the cylinder, against the front of the cylinder. This also compresses the front "volute" spring pulling the whole cylinder forwards. That action pulls the rear wheel down on the same side via the rear spring assembly and pull rod. When the rear wheel meets that bump a moment later, it does the same in reverse, keeping the car level front to rear. When both springs are compressed on one side when travelling around a bend, or front and rear wheels hit bumps simultaneously, the equal and opposite forces applied to the front and rear spring assemblies reduce the interconnection. It reduces pitching, which is a particular problem of soft car suspension.
The swinging arms are mounted with large bearings to "cross tubes" that run side to side across the chassis; combined with the effects of all-independent soft springing and excellent damping, keeps the road wheels in contact with the road surface and parallel to each other across the axles at high angles of body roll. A larger than conventional steering castor angle, ensures that the front wheels are closer to vertical than the rears, when cornering hard with a lot of body roll. The soft springing, long suspension travel and the use of leading and trailing arms means that as the body rolls during cornering the wheelbase on the inside of the corner increases while the wheelbase on the outside of the corner decreases. As the corning forces put more of the car's weight on the inside pair of wheels the wheelbase extends in proportion, keeping the car's weight balance and centre of grip constant. promoting excellent road holding. The other key factor in the quality of its road holding is the very low and forward centre of gravity, provided by the position of the engine and transmission.
The suspension also automatically accommodates differing payloads in the car- with four people and cargo on board the wheelbase increases by around 4 cm as the suspension deflects, and the castor angle of the front wheels increases by as much as 8 degrees thus ensuring that ride quality, handling and road holding are almost unaffected by the additional weight. On early cars friction dampers (like a dry version of a multi-plate clutch design) were fitted at the mountings of the front and rear swinging arms to the cross-tubes. Because the rear brakes were outboard, they had extra tuned mass dampers to damp wheel bounce from the extra unsprung mass. Later models had tuned mass dampers ("batteurs") at the front (because the leading arm had more inertia and "bump/thump" than the trailing arm), with hydraulic telescopic dampers / shock absorbers front and rear. The uprated hydraulic damping obviated the need for the rear inertia dampers. It was designed to be a comfortable ride by matching the frequencies encountered in human bipedal motion.
This suspension design ensured the road wheels followed ground contours underneath them closely, while insulating the vehicle from shocks, enabling the 2CV to be driven over a ploughed field without breaking any eggs, as its design brief required. More importantly it could comfortably and safely drive at reasonable speed, along the ill-maintained and war-damaged post-war French Routes Nationales. It was commonly driven "Pied au Plancher" — "foot to the floor" by their peasant owners.
FRONT-WHEEL DRIVE AND GEARBOX
Citroën had developed expertise with front-wheel drive due to the pioneering Traction Avant, which was the first mass-produced steel monocoque front-wheel-drive car in the world. The 2CV was originally equipped with a sliding splined joint, and twin Hookes type universal joints on its driveshafts; later models used constant velocity joints and a sliding splined joint.
The gearbox was a four-speed manual transmission, an advanced feature on an inexpensive car at the time. The gear stick came horizontally out of the dashboard with the handle curved upwards. It had a strange shift pattern: the first was back on the left, the second and third were inline, and the fourth (or the S) could be engaged only by turning the lever to the right from the third. Reverse was opposite first. The idea was to put the most used gears opposite each other — for parking, first and reverse; for normal driving, second and third. This layout was adopted from the H-van's three-speed gearbox.
OTHER
The windscreen wipers were powered by a purely mechanical system: a cable connected to the transmission; to reduce cost, this cable also powered the speedometer. The wipers' speed was therefore dependent on car speed. When the car was waiting at a crossroad, the wipers were not powered; thus, a handle under the speedometer allowed them to be operated by hand. From 1962, the wipers were powered by a single-speed electric motor. The car came with only a speedometer and an ammeter.
The 2CV design predates the invention of disc brake, so 1948–1981 cars have drum brakes on all four wheels. In October 1981, front disc brakes were fitted. Disc brake cars use green LHM fluid – a mineral oil – which is not compatible with standard glycol brake fluid.
ENGINES
The engine was designed by Walter Becchia and Lucien Gerard, with a nod to the classic BMW boxer motorcycle engine. It was an air-cooled, flat-twin, four-stroke, 375 cc engine with pushrod operated overhead valves and a hemispherical combustion chamber. The earliest model developed 9 PS (6.6 kW) DIN (6.5 kW). A 425 cc engine was introduced in 1955, followed in 1968 by a 602 cc one giving 28 bhp (21 kW) at 7000 rpm. With the 602 cc engine, the tax classification of the car changed so that it became a 3CV, but the name remained unchanged. A 435 cc engine was introduced at the same time to replace the 425 cc; the 435 cc engine car was named 2CV 4 while the 602 cc took the name 2CV 6 (a variant in Argentina took the name 3CV). The 602 cc engine evolved to the M28 33 bhp (25 kW) in 1970; this was the most powerful engine fitted to the 2CV. A new 602 cc giving 29 bhp (22 kW) at a slower 5,750 rpm was introduced in 1979. This engine was less powerful, and more efficient, allowing lower fuel consumption and better top speed, but decreased acceleration. All 2CVs with the M28 engine can run on unleaded petrol.
The 2CV used the wasted spark ignition system for simplicity and reliability and had only speed-controlled ignition timing, no vacuum advance taking account of engine load.
Unlike other air-cooled cars (such as the Volkswagen Beetle and the Fiat 500) the 2CV's engine had no thermostat valve in its oil system. The engine needed more time for oil to reach normal operating temperature in cold weather. All the oil passed through an oil cooler behind the fan and received the full cooling effect regardless of the ambient temperature. This removes the risk of overheating from a jammed thermostat that can afflict water- and air-cooled engines and the engine can withstand many hours of running under heavy load at high engine speeds even in hot weather. To prevent the engine running cool in cold weather (and to improve the output of the cabin heater) all 2CVs were supplied with a grille blind (canvas on early cars and a clip-on plastic item called a "muff" in the owner's handbook, on later ones) which blocked around half the aperture to reduce the flow of air to the engine.
The engine's design concentrated on the reduction of moving parts. The cooling fan and dynamo were built integrally with the one-piece crankshaft, removing the need for drive belts. The use of gaskets, seen as another potential weak point for failure and leaks, was also kept to a minimum. The cylinder heads are mated to the cylinder barrels by lapped joints with extremely fine tolerances, as are the two halves of the crankcase and other surface-to-surface joints.
As well as the close tolerances between parts, the engine's lack of gaskets was made possible by a unique crankcase ventilation system. On any 2-cylinder boxer engine such as the 2CV's, the volume of the crankcase reduces by the cubic capacity of the engine when the pistons move together. This, combined with the inevitable small amount of "leakage" of combustion gases past the pistons leads to a positive pressure in the crankcase which must be removed in the interests of engine efficiency and to prevent oil and gas leaks. The 2CV's engine has a combined engine "breather" and oil filler assembly which contains a series of rubber reed valves. These allow positive pressure to escape the crankcase (to the engine air intake to be recirculated) but close when the pressure in the crankcase drops as the pistons move apart. Because gases are expelled but not admitted this creates a slight vacuum in the crankcase so that any weak joint or failed seal causes air to be sucked in rather than allowing oil to leak out.
These design features made the 2CV engine highly reliable; test engines were run at full speed for 1000 hours at a time, equivalent to driving 80,000 km at full throttle. They also meant that the engine was "sealed for life" — for example, replacing the big-end bearings required specialised equipment to dismantle and reassemble the built-up crankshaft, and as this was often not available the entire crankshaft had to be replaced. The engine is very under-stressed and long-lived, so this is not a major issue.
If the starter motor or battery failed, the 2CV had the option of hand-cranking, the jack handle serving as starting handle through dogs on the front of the crankshaft at the centre of the fan. This feature, once universal on cars and still common in 1948 when the 2CV was introduced, was kept until the end of production in 1990.
PERFORMANCE
In relation to the 2CV's performance and acceleration, it was joked that it went "from 0–60 km/h in one day". The original 1948 model that produced 9 hp had a 0–40 time of 42.4 seconds and a top speed of 64 km/h, far below the speeds necessary for North American highways or the German Autobahns of the day. The top speed increased with engine size to 80 km/h in 1955, 84 km/h in 1962, 100 km/h in 1970, and 115 km/h in 1981.
The last evolution of the 2CV engine was the Citroën Visa flat-2, a 652 cc featuring electronic ignition. Citroën never sold this engine in the 2CV, but some enthusiasts have converted their 2CVs to 652 engines, or even transplanted Citroën GS or GSA flat-four engines and gearboxes.
In the mid-1980s Car magazine editor Steve Cropley ran and reported on a turbocharged 602 cc 2CV that was developed by engineer Richard Wilsher.
END OF PRODUCTION
The 2CV was produced for 42 years, the model finally succumbing to customer demands for speed, in which this ancient design had fallen significantly behind modern cars, and safety. Although the front of the chassis was designed to fold up, to form a crumple zone according to a 1984 Citroën brochure, in common with other small cars of its era its crashworhiness was very poor by modern standards. (The drive for improved safety in Europe happened from the 1990s onwards, and accelerated with the 1997 advent of Euro NCAP.) Its advanced underlying engineering was ignored or misunderstood by the public, being clothed in an anachronistic body. It was the butt of many a joke, especially by Jasper Carrott in the UK.
Citroën had attempted to replace the ultra-utilitarian 2CV several times (with the Dyane, Visa, and the AX). Its comically antiquated appearance became an advantage to the car, and it became a niche product which sold because it was different from anything else on sale. Because of its down-to-earth economy car style, it became popular with people who wanted to distance themselves from mainstream consumerism — "hippies" — and also with environmentalists.
Although not a replacement for the 2CV, the AX supermini, a conventional urban runabout, unremarkable apart from its exceptional lightness, seemed to address the car makers' requirements at the entry level in the early 1990s. Officially, the last 2CV, a Charleston, which was reserved for Mangualde's plant manager, rolled off the Portuguese production line on 27 July 1990, although five additional 2CV Spécials were produced afterwards.[citation needed]
In all a total of 3,867,932 2CVs were produced. Including the commercial versions of the 2CV, Dyane, Méhari, FAF, and Ami variants, the 2CV's underpinnings spawned 8,830,679 vehicles.
The 2CV was outlived by contemporaries such as the Mini (out of production in 2000), Volkswagen Beetle (2003), Renault 4 (1992), Volkswagen Type 2 (2013) and Hindustan Ambassador (originally a 1950s Morris Oxford), (2014).
CONTINUED POPULARITY
The Chrysler CCV or Composite Concept Vehicle developed in the mid-1990s is a concept car designed to illustrate new manufacturing methods suitable for developing countries. The car is a tall, roomy four-door sedan of small dimensions. The designers at Chrysler said they were inspired to create a modernised 2CV.
The company Sorevie of Lodève was building 2CVs until 2002. The cars were built from scratch using mostly new parts. But as the 2CV no longer complied with safety regulations, the cars were sold as second-hand cars using chassis and engine numbers from old 2CVs.
The long-running 2CV circuit racing series organized by The Classic 2CV Racing Club continues to be popular in the UK.
English nicknames include "Flying Dustbin", "Tin Snail", "Dolly", "Tortoise"
WIKIPEDIA
I really like to use metal subject in my macro-tests. Their surface usually contains a lot of scratches and marks, so shows the sharpness very well. Metal has also very good capability of reflection, so it's perfect specimen to adjust light in tests. In this case I used keys as an example.
This is the billiard room, which has another fine ceiling by Capability Brown. On the wall are portraits of the great and good (and sometimes not so good) while below the oval ones are members of the Little Bedlam Club, a 17th-century drinking and gaming club.
The early work of Robert Adam and Capability Brown...in the process of restoration after suffering mixed fortunes and varied uses by many owners since the 1940s....at least its in the expert hands of the Trust now
Croome Court is a mid 18th century Neo-Palladian mansion surrounded by an extensive landscaped parkland at Croome D'Abitot, near Pershore in south Worcestershire. The mansion and park were designed by Lancelot "Capability" Brown for George Coventry, 6th Earl of Coventry, and was Brown's first landscape design and first major architectural project. Some of the internal rooms of the mansion were designed by Robert Adam.
The mansion house is owned by Croome Heritage Trust, and is leased to the National Trust who operate it, along with the surrounding parkland, as a tourist attraction. The National Trust own the surrounding parkland, which is also open to the public.
Location[edit]
Croome Court is located near to Croome D'Abitot, in Worcestershire,[1] near Pirton, Worcestershire.[2] The wider estate was established on lands that were once part of the royal forest of Horewell.[3] Traces of these older landscapes, such as unimproved commons and ancient woodlands, can be found across the former Croome Estate.[4]
House[edit]
Croome Court South Portico
History[edit]
The foundations and core of Croome Court, including the central chimney stack structure, date back to the early 1640s.[5] Substantial changes to this early house were made by Gilbert Coventry, 4th Earl of Coventry.[6]
In 1751, George Coventry, the 6th Earl, inherited the estate, along with the existing Jacobean house. He commissioned Lancelot "Capability" Brown, with the assistance of Sanderson Miller, to redesign the house and estate.[7][1] It was Brown's "first flight into the realms of architecture" and a "rare example of his architectural work",[8] and it is an important and seminal work.[9] It was built between 1751 and 1752, and it and Hagley Hall are considered to be the finest examples of Neo-Palladian architecture in Worcestershire. Notable Neo-Palladian features incorporated into Croome Court include the plain exterior and the corner towers with pyramidal roofs (a feature first used by Inigo Jones in the design of Wilton House in Wiltshire).[1] Robert Adam worked on the interior of the building from 1760 onwards.[10]
The house has been visited by George III,[2][11] as well as Queen Victoria[7] during summers when she was a child, and George V (then Duke of York).[11]
A jam factory was built by the 9th Earl of Coventry, near to Pershore railway station, in about 1880, to provide a market for Vale of Evesham fruit growers in times of surplus. Although the Croome connection with jam making had ceased, during the First World War, the building was leased by the Croome Estate Trust to the Huddersfield Fruit Preserving Company as a pulping station.[12]
The First World War deeply affected Croome, with many local casualties, although the house was not requisitioned for the war effort. This is possibly because it was the home of the Lord Lieutenant of the County, who needed a residence for his many official engagements.[13]
During the Second World War Croome Court was requisitioned by the Ministry of Works and leased for a year to the Dutch Government as a possible refuge for Queen Wilhelmina of the Netherlands; to escape the Nazi occupation of the Netherlands. However, evidence shows that they stayed two weeks at the most, perhaps because of the noise and fear created by the proximity of Defford Aerodrome. They later emigrated to Canada.[14]
In 1948 the Croome Estate Trust sold the Court, along with 38 acres (15 ha) of land, to the Roman Catholic Archdiocese of Birmingham, and the mansion became St Joseph's Special School, which was run by nuns[15] from 1950[11] until 1979.[15]
The house was listed on 11 August 1952; it is currently Grade I listed.[10]
In 1979 the hall was taken over by the International Society for Krishna Consciousness (Hare Krishna movement), who used it as their UK headquarters and a training college[16] called Chaitanya College,[15] run by 25 members of the movement.[16] During their tenure they repainted the Dining Room.[17] In 1984 they had to leave the estate for financial reasons. They held a festival at the hall in 2011.[16]
From 1984 onwards various owners tried to use the property as a training centre; apartments; a restaurant and conference centre; and a hotel and golf course,[15] before once more becoming a private family home,[2][15] with outbuildings converted to private houses.[15]
The house was purchased by the Croome Heritage Trust, a registered charity,[18] in October 2007,[19] and it is now managed by the National Trust as a tourist attraction. It opened to the public in September 2009, at which point six of the rooms had restored, costing £400,000, including the Saloon. It was estimated that another £4 million[2][20] to £4.8 million would be needed to restore the entire building. Fundraising activities for the restoration included a 2011 raffle for a Morgan sports car organised by Lord and Lady Flight. After the restoration is complete, a 999-year lease on the building will be granted to the National Trust.[21] An oral history project to record recollections about Croome was funded by the Heritage Lottery Fund.[15] As of 2009, the service wing was empty and in need of substantial repair.[22]
Exterior[edit]
The mansion is faced with Bath stone,[7] limestone ashlar, and has both north and south facing fronts. It has a basement and two stories, with three stories in the end pavilions. A slate roof, with pyramid roofs over the corner towers, tops the building, along with three pair-linked chimneys along the axis of the house.[10]
Both fronts have 11 bays, split into three central sets of three each, and one additional bay each side. The north face has a pedimented centre, with two balustraded staircases leading to a Roman Doric doorcase. The south face has a projecting Ionic tetrastyle portico and Venetian windows. It has a broad staircase, with cast stone sphinxes on each side, leading to a south door topped with a cornice on consoles. The wings have modillion cornice and balustrade.[10]
A two-story L-shaped service wing is attached to the east side of the mansion. It is made of red brick and stone, with slate roofs.[10] It was designed by Capability Brown in 1751-2.[22] On the far side of the service wing, a wall connects it to a stable court.[10]
Interior[edit]
The interior of the house was designed partially by Capability Brown, with plasterwork by G. Vassalli, and partially by Robert Adam, with plasterwork by J. Rose Jr. It has a central spine corridor. A stone staircase, with iron balusters, is at the east end.[10]
The entrance hall is on the north side of the building, and has four fluted Doric columns, along with moulded doorcases. To the east of the entrance hall is the dining room, which has a plaster ceiling and cornice, while to the west is a billiard room, featuring fielded panelling, a plaster cornice, and a rococo fireplace. The three rooms were probably decorated around 1758-59 by Capability Brown.[10] The dining room was vibrantly repainted by the Hare Krishnas in the 1970s-80s.[17]
The central room on the south side is a saloon, probably by Brown and Vassalli. It has an elaborate ceiling, with three panels, deep coving, and a cornice, along with two Ionic fireplaces, and Palladian doorcases.[10] George III was entertained by George Coventry, the 6th Earl, in the house's Saloon.[2] A drawing room is to the west of the saloon, and features rococo plasterwork and a marble fireplace.[10]
To the east of the saloon is the Tapestry Room.[10] This was designed in 1763-71, based on a design by Robert Adam, and contained tapestries and furniture covers possibly designed by Jacques Germain Soufflot, and made by Manufacture Nationale des Gobelins.[23] Around 1902 the ninth Earl sold the tapestries and seating to a Parisian dealer. In 1949 the Samuel H. Kress Foundation purchased the ceiling, floor, mantlepiece, chair rails, doors and the door surrounds, which were donated to the Metropolitan Museum of Art, New York, in 1958. In 1959 the Kress Foundation also helped the Metropolitan Museum acquire the chair and sofa frames, which they recovered using the original tapestry seats.[7][23] A copy of the ceiling was installed in place of the original.[10] As of 2016, the room is displayed as it would have looked after the tapestries had been sold, with a jug and ewer on display as the only original decoration of the room that remains in it. The adjacent library room is used to explain what happened to the tapestry room;[17] the former library was designed by Adam, and was dismantled except for the marble fireplace.[10]
At the west side of the building is a long gallery,[10] which was designed by Robert Adam and installed between 1761 and 1766. It is the best preserved of the original interior (little of the rest has survived in situ).[1] It has an octagonal panelled ceiling, and plaster reliefs of griffins. A half-hexagonal bay faces the garden. The room also contains a marble caryatid fireplace designed by J Wilton.[10] As of 2016, modern sculptures are displayed in empty niches along the Long Gallery
wikipedia
Taken on May Day in Church Stretton, Shropshire. Rectory Wood once formed part of the grounds of the Rectory in Church Stretton. In around 1775 the owner, James Mainwaring, made great changes to create a designed woodland landscaped garden. It is believed that Lancelot 'Capability' Brown, a friend of Mainwaring and arguably the greatest british landscape gardener of the Georgian era, influenced the design here at Rectory Wood.
Lancelot Brown acquired the name "Capability" from his habit of telling clients that their gardens had "great capabilites".
Lancelot Brown, however, describled himself as a "place maker" not a landscape gardener.
The bluebells here are beautiful.
A Fountain at Harewood House, near Leeds, West Yorkshire.
Harewood House is a Grade 1 Country House near Leeds in West Yorkshire.
It was designed by architects John Carr and Robert Adam and built between 1759 and 1771 for wealthy plantation and slave owner Edwin Lascelles - the 1st Baron Harewood, and is still home to the Lascelles family.
The 1000 acre grounds were designed by Capability Brown.
The house is one of the ten 'Treasure Houses of England'.
A spectacular house and grounds that is well worth a visit, but uncomfortable about the source of the wealth that built it.
+++ DISCLAIMER +++
Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!
Some background:
After the success of the Soviet Union’s first carrier ship, the Moskva Class (Projekt 1123, also called „Кондор“/„Kondor“) cruisers in the mid 1960s, the country became more ambitious. This resulted in Project 1153 Orel (Russian: Орёл, Eagle), a planned 1970s-era Soviet program to give the Soviet Navy a true blue water aviation capability. Project Orel would have resulted in a program very similar to the aircraft carriers available to the U.S. Navy. The ship would have been about 75-80,000 tons displacement, with a nuclear power plant and carried about 70 aircraft launched via steam catapults – the first Soviet aircraft carrier that would be able to deploy fixed-wing aircraft.
Beyond this core capability, the Orel carrier was designed with a large offensive capability with the ship mounts including 24 vertical launch tubes for anti-ship cruise missiles. In the USSR it was actually classified as the "large cruiser with aircraft armament".
Anyway, the carrier needed appropriate aircraft, and in order to develop a the aircraft major design bureaus were asked to submit ideas and proposals in 1959. OKB Yakovlev and MiG responded. While Yakovlev concentrated on the Yak-36 VTOL design that could also be deployed aboard of smaller ships without catapult and arrester equipment, Mikoyan-Gurevich looked at navalized variants of existing or projected aircraft.
While land-based fighters went through a remarkable performance improvement during the 60ies, OKB MiG considered a robust aircraft with proven systems and – foremost – two engines to be the best start for the Soviet Union’s first naval fighter. “Learning by doing”, the gathered experience would then be used in a dedicated new design that would be ready in the mid 70ies when Project 1153 was ready for service, too.
Internally designated “I-SK” or “SK-01” (Samolyot Korabelniy = carrier-borne aircraft), the naval fighter was based on the MiG-19 (NATO: Farmer), which had been in production in the USSR since 1954.
Faster and more modern types like the MiG-21 were rejected for a naval conversion because of their poor take-off performance, uncertain aerodynamics in the naval environment and lack of ruggedness. The MiG-19 also offered the benefit of relatively compact dimensions, as well as a structure that would carry the desired two engines.
Several innovations had to be addresses:
- A new wing for improved low speed handling
- Improvement of the landing gear and internal structures for carrier operations
- Development of a wing folding mechanism
- Integration of arrester hook and catapult launch devices into the structure
- Protection of structure, engine and equipment from the aggressive naval environment
- Improvement of the pilot’s field of view for carrier landings
- Improved avionics, esp. for navigation
Work on the SK-01 started in 1960, and by 1962 a heavily redesigned MiG-19 was ready as a mock-up for inspection and further approval. The “new” aircraft shared the outlines with the land-based MiG-19, but the nose section was completely new and shared a certain similarity to the experimental “Aircraft SN”, a MiG-17 derivative with side air intakes and a solid nose that carried a. Unlike the latter, the cockpit had been moved forward, which offered, together with an enlarged canopy and a short nose, an excellent field of view for the pilot.
On the SK-01 the air intakes with short splitter plates were re-located to the fuselage flanks underneath the cockpit. In order to avoid gun smoke ingestion problems (and the lack of space in the nose for any equipment except for a small SRD-3 Grad gun ranging radar, coupled with an ASP-5N computing gun-sight), the SK-01’s internal armament, a pair of NR-30 cannon, was placed in the wing roots.
The wing itself was another major modification, it featured a reduced sweep of only 33° at ¼ chord angle (compared to the MiG-19’s original 55°). Four wing hardpoints, outside of the landing gear wells, could carry a modest ordnance payload, including rocket and gun pods, unguided missiles, iron bombs and up to four Vympel K-13 AAMs.
Outside of these pylons, the wings featured a folding mechanism that allowed the wing span to be reduced from 10 m to 6.5 m for stowage. The fin remained unchanged, but the stabilizers had a reduced sweep, too.
The single ventral fin of the MiG-19 gave way to a fairing for a massive, semi-retractable arrester hook, flanked by a pair of smaller fins. The landing gear was beefed up, too, with a stronger suspension. Catapult launch from deck was to be realized through expandable cables that were attached onto massive hooks under the fuselage.
The SK-01 received a “thumbs up” in March 1962 and three prototypes, powered by special Sorokin R3M-28 engines, derivatives of the MiG-19's RB-9 that were adapted to the naval environment, were created and tested until 1965, when the type – now designated MiG-SK – went through State Acceptance Trials, including simulated landing tests on an “unsinkalble carrier” dummy, a modified part of the runway at Air Base at the Western coast of the Caspian Sea. Not only flight tests were conducted at Kaspiysk, but also different layouts for landing cables were tested and optimized as well. Furthermore, on a special platform at the coast, an experimental steam catapult went through trials, even though no aircraft starts were made from it – but weights hauled out into the sea.
Anyway, the flight tests and the landing performance on the simulated carrier deck were successful, and while the MiG-SK (the machine differed from the MiG-19 so much that it was not recognized as an official MiG-19 variant) was not an outstanding combat aircraft, rather a technology carrier with field use capabilities.
The MiG-SK’s performance was good enough to earn OKB MiG an initial production run of 20 aircraft, primarily intended for training and development units, since the whole infrastructure and procedures for naval aviation from a carrier had to be developed from scratch. These machines were built at slow pace until 1968 and trials were carried out in the vicinity of the Black Sea and the Caspian Sea.
The MiG-SK successfully remained hidden from the public, since the Soviet Navy did not want to give away its plans for a CTOL carrier. Spy flights of balloons and aircraft recognized the MiG-SK, but the type was mistaken as MiG-17 fighters. Consequently, no NATO codename was ever allocated.
Alas, the future of the Soviet, carrier-borne fixed wing aircraft was not bright: Laid down in in 1970, the Kiev-class aircraft carriers (also known as Project 1143 or as the Krechyet (Gyrfalcon) class) were the first class of fixed-wing aircraft carriers to be built in the Soviet Union, and they entered service, together with the Yak-38 (Forger) VTOL fighter, in 1973. This weapon system already offered a combat performance similar to the MiG-SK, and the VTOL concept rendered the need for catapult launch and deck landing capability obsolete.
OKB MiG still tried to lobby for a CTOL aircraft (in the meantime, the swing-wing MiG-23 was on the drawing board, as well as a projected, navalized multi-purpose derivative, the MiG-23K), but to no avail.
Furthermore, carrier Project 1153 was cancelled in October 1978 as being too expensive, and a program for a smaller ship called Project 11435, more V/STOL-aircraft-oriented, was developed instead; in its initial stage, a version of 65,000 tons and 52 aircraft was proposed, but eventually an even smaller ship was built in the form of the Kuznetsov-class aircraft carriers in 1985, outfitted with a 12-degree ski-jump bow flight deck instead of using complex aircraft catapults. This CTOL carrier was finally equipped with navalized Su-33, MiG-29 and Su-25 aircraft – and the MiG-SK paved the early way to these shipboard fighters, especially the MiG-29K.
General characteristics:
Crew: One
Length: 13.28 m (43 ft 6 in)
Wingspan: 10.39 m (34 ft)
Height: 3.9 m (12 ft 10 in)
Wing area: 22.6 m² (242.5 ft²)
Empty weight: 5.172 kg (11,392 lb)
Max. take-off weight: 7,560 kg (16,632 lb)
Powerplant:
2× Sorokin R3M-28 turbojets afterburning turbojets, rated at 33.8 kN (7,605 lbf) each
Performance:
Maximum speed: 1,145 km/h (618 knots, 711 mph) at 3,000 m (10,000 ft)
Range: 2,060 km (1,111 nmi, 1,280 mi) with drop tanks
Service ceiling: 17,500 m (57,400 ft)
Rate of climb: 180 m/s (35,425 ft/min)
Wing loading: 302.4 kg/m² (61.6 lb/ft²)
Thrust/weight: 0.86
Armament:
2x 30 mm NR-30 cannons in the wing roots with 75 RPG
4x underwing pylons, with a maximum load of 1.000 kg (2.205 lb)
The kit and its assembly:
This kitbash creation was spawned by thoughts concerning the Soviet Naval Aviation and its lack of CTOL aircraft carriers until the 1980ies and kicked-off by a CG rendition of a navalized MiG-17 from fellow member SPINNERS at whatifmodelers.com, posted a couple of months ago. I liked this idea, and at first I wanted to convert a MiG-17 with a solid nose as a dedicated carrier aircraft. But the more I thought about it and did historic research, the less probable this concept appeared to me: the MiG-17 was simply too old to match Soviet plans for a carrier ship, at least with the real world as reference.
A plausible alternative was the MiG-19, esp. with its twin-engine layout, even though the highly swept wings and the associated high start and landing speeds would be rather inappropriate for a shipborne fighter. Anyway, a MiG-21 was even less suitable, and I eventually took the Farmer as conversion basis, since it would also fit into the historic time frame between the late 60ies and the mid-70ies.
In this case, the basis is a Plastyk MiG-19 kit, one of the many Eastern European re-incarnations of the vintage KP kit. This cheap re-issue became a positive surprise, because any former raised panel and rivet details have disappeared and were replaced with sound, recessed engravings. The kit is still a bit clumsy, the walls are very thick (esp. the canopy – maybe 2mm!), but IMHO it’s a considerable improvement with acceptable fit, even though there are some sink holes and some nasty surprises (in my case, for instance, the stabilizer fins would not match with the rear fuselage at all, and you basically need putty everywhere).
Not much from the Plastyk kit was taken over, though: only the fuselage’s rear two-thirds were used, some landing gear parts as well as fin and the horizontal stabilizers. The latter were heavily modified and reduced in sweep in order to match new wings from a Hobby Boss MiG-15 (the parts were cut into three pieces each and then set back together again).
Furthermore, the complete front section from a Novo Supermarine Attacker was transplanted, because its short nose and the high cockpit are perfect parts for a carrier aircraft. The Attacker’s front end, including the air intakes, fits almost perfectly onto the round MiG-19 forward fuselage, only little body work was necessary. A complete cockpit tub and a new seat were implanted, as well as a front landing gear well and walls inside of the (otherwise empty) air intakes. The jet exhausts were drilled open, too, and afterburner dummies added. Simple jobs.
On the other side, the wings were trickier than expected. The MiG-19 kit comes with voluminous and massive wing root fairings, probably aerodynamic bodies for some area-ruling. I decided to keep them, but this caused some unexpected troubles…
The MiG-15 wings’ position, considerably further back due to the reduced sweep angle, was deduced from the relative MiG-19’s landing gear position. A lot of sculpting and body work followed, and after the wings were finally in place I recognized that the aforementioned, thick wing root fairings had reduced the wing sweep – basically not a bad thing, but with the inconvenient side effect that the original wing MiG-15 fences were not parallel to the fuselage anymore, looking rather awkward! What to do? Grrrr…. I could not leave it that way, so I scraped them away and replaced with them with four scratched substitutes (from styrene profiles), moving the outer pair towards the wing folding mechanism.
Under the wings, four new pylons were added (two from an IAI Kfir, two from a Su-22) and the ordnance gathered from the scrap box – bombs and rocket pods formerly belonged to a Kangnam/Revell Yak-38.
The landing gear was raised by ~2mm for a higher stance on the ground. The original, thick central fin was reduced in length, so that it could become a plausible attachment point for an arrester hook (also from the spares box), and a pair of splayed stabilizer fins was added as a compensation. Finally, some of the OOB air scoops were placed all round the hull and some pitots, antennae and a gun camera fairing added.
Painting and markings:
This whif was to look naval at first sight, so I referred to the early Yak-38 VTOL aircraft and their rather minimalistic paint scheme in an overall dull blue. The green underside, seen on many service aircraft, was AFAIK a (later) protective coating – an obsolete detail for a CTOL aircraft.
Hence, all upper surfaces and the fuselage were painted in a uniform “Field Blue” (Tamiya XF-50). It’s a bit dark, but I have used this unique, petrol blue tone many moons ago on a real world Kangnam Forger where it looks pretty good, and in this case the surface was furthermore shaded with Humbrol 96 and 126 after a black in wash.
For some contrast I painted the undersides of the wings and stabilizers as well as a fuselage section between the wings in a pale grey (Humbrol 167), seen on one of the Yak-38 prototypes. Not very obvious, but at least the aircraft did not end up in a boring, uniform color.
The interior was painted in blue-gray (PRU Blue, shaded with Humbrol 87) while the landing gear wells became Aluminum (Humbrol 56). The wheel discs became bright green, just in order to keep in style and as a colorful contrast, and some di-electric panels and covers became very light grey or bright green. For some color contrast, the anti-flutter weight tips on the stabilizers as well as the pylons’ front ends were painted bright red.
The markings/decals reflect the early Soviet Navy style, with simple Red Stars, large yellow tactical codes and some high contrast warning stencils, taken from the remains of a Yak-38 sheet (American Revell re-release of the Kangnam kit).
Finally, after some soot stains with graphite around the gun muzzles and the air bleed doors, the kit was sealed with a coat of semi-matt acrylic varnish and some matt accents (anti-glare panel, radomes).
A simple idea that turned out to be more complex than expected, due to the wing fence troubles. But I am happy that the Attacker nose could be so easily transplanted, it changes the MiG-19’s look considerably, as well as the wings with (much) less sweep angle.
The aircraft looks familiar, but you only recognize at second glance that it is more than just a MiG-19 with a solid nose. The thing looks pretty retro, reminds me a bit of the Supermarine Scimitar (dunno?), and IMHO it appears more Chinese than Soviet (maybe because the layout reminds a lot of the Q-5 fighter bomber)? It could even, with appropriate markings, be a Luft ’46 design?
Croome Court is a mid 18th century Neo-Palladian mansion surrounded by an extensive landscaped parkland at Croome D'Abitot, near Pershore in south Worcestershire. The mansion and park were designed by Lancelot "Capability" Brown for George Coventry, 6th Earl of Coventry, and was Brown's first landscape design and first major architectural project. Some of the internal rooms of the mansion were designed by Robert Adam.
The mansion house is owned by Croome Heritage Trust, and is leased to the National Trust who operate it, along with the surrounding parkland, as a tourist attraction. The National Trust own the surrounding parkland, which is also open to the public.
Location[edit]
Croome Court is located near to Croome D'Abitot, in Worcestershire,[1] near Pirton, Worcestershire.[2] The wider estate was established on lands that were once part of the royal forest of Horewell.[3] Traces of these older landscapes, such as unimproved commons and ancient woodlands, can be found across the former Croome Estate.[4]
House[edit]
Croome Court South Portico
History[edit]
The foundations and core of Croome Court, including the central chimney stack structure, date back to the early 1640s.[5] Substantial changes to this early house were made by Gilbert Coventry, 4th Earl of Coventry.[6]
In 1751, George Coventry, the 6th Earl, inherited the estate, along with the existing Jacobean house. He commissioned Lancelot "Capability" Brown, with the assistance of Sanderson Miller, to redesign the house and estate.[7][1] It was Brown's "first flight into the realms of architecture" and a "rare example of his architectural work",[8] and it is an important and seminal work.[9] It was built between 1751 and 1752, and it and Hagley Hall are considered to be the finest examples of Neo-Palladian architecture in Worcestershire. Notable Neo-Palladian features incorporated into Croome Court include the plain exterior and the corner towers with pyramidal roofs (a feature first used by Inigo Jones in the design of Wilton House in Wiltshire).[1] Robert Adam worked on the interior of the building from 1760 onwards.[10]
The house has been visited by George III,[2][11] as well as Queen Victoria[7] during summers when she was a child, and George V (then Duke of York).[11]
A jam factory was built by the 9th Earl of Coventry, near to Pershore railway station, in about 1880, to provide a market for Vale of Evesham fruit growers in times of surplus. Although the Croome connection with jam making had ceased, during the First World War, the building was leased by the Croome Estate Trust to the Huddersfield Fruit Preserving Company as a pulping station.[12]
The First World War deeply affected Croome, with many local casualties, although the house was not requisitioned for the war effort. This is possibly because it was the home of the Lord Lieutenant of the County, who needed a residence for his many official engagements.[13]
During the Second World War Croome Court was requisitioned by the Ministry of Works and leased for a year to the Dutch Government as a possible refuge for Queen Wilhelmina of the Netherlands; to escape the Nazi occupation of the Netherlands. However, evidence shows that they stayed two weeks at the most, perhaps because of the noise and fear created by the proximity of Defford Aerodrome. They later emigrated to Canada.[14]
In 1948 the Croome Estate Trust sold the Court, along with 38 acres (15 ha) of land, to the Roman Catholic Archdiocese of Birmingham, and the mansion became St Joseph's Special School, which was run by nuns[15] from 1950[11] until 1979.[15]
The house was listed on 11 August 1952; it is currently Grade I listed.[10]
In 1979 the hall was taken over by the International Society for Krishna Consciousness (Hare Krishna movement), who used it as their UK headquarters and a training college[16] called Chaitanya College,[15] run by 25 members of the movement.[16] During their tenure they repainted the Dining Room.[17] In 1984 they had to leave the estate for financial reasons. They held a festival at the hall in 2011.[16]
From 1984 onwards various owners tried to use the property as a training centre; apartments; a restaurant and conference centre; and a hotel and golf course,[15] before once more becoming a private family home,[2][15] with outbuildings converted to private houses.[15]
The house was purchased by the Croome Heritage Trust, a registered charity,[18] in October 2007,[19] and it is now managed by the National Trust as a tourist attraction. It opened to the public in September 2009, at which point six of the rooms had restored, costing £400,000, including the Saloon. It was estimated that another £4 million[2][20] to £4.8 million would be needed to restore the entire building. Fundraising activities for the restoration included a 2011 raffle for a Morgan sports car organised by Lord and Lady Flight. After the restoration is complete, a 999-year lease on the building will be granted to the National Trust.[21] An oral history project to record recollections about Croome was funded by the Heritage Lottery Fund.[15] As of 2009, the service wing was empty and in need of substantial repair.[22]
Exterior[edit]
The mansion is faced with Bath stone,[7] limestone ashlar, and has both north and south facing fronts. It has a basement and two stories, with three stories in the end pavilions. A slate roof, with pyramid roofs over the corner towers, tops the building, along with three pair-linked chimneys along the axis of the house.[10]
Both fronts have 11 bays, split into three central sets of three each, and one additional bay each side. The north face has a pedimented centre, with two balustraded staircases leading to a Roman Doric doorcase. The south face has a projecting Ionic tetrastyle portico and Venetian windows. It has a broad staircase, with cast stone sphinxes on each side, leading to a south door topped with a cornice on consoles. The wings have modillion cornice and balustrade.[10]
A two-story L-shaped service wing is attached to the east side of the mansion. It is made of red brick and stone, with slate roofs.[10] It was designed by Capability Brown in 1751-2.[22] On the far side of the service wing, a wall connects it to a stable court.[10]
Interior[edit]
The interior of the house was designed partially by Capability Brown, with plasterwork by G. Vassalli, and partially by Robert Adam, with plasterwork by J. Rose Jr. It has a central spine corridor. A stone staircase, with iron balusters, is at the east end.[10]
The entrance hall is on the north side of the building, and has four fluted Doric columns, along with moulded doorcases. To the east of the entrance hall is the dining room, which has a plaster ceiling and cornice, while to the west is a billiard room, featuring fielded panelling, a plaster cornice, and a rococo fireplace. The three rooms were probably decorated around 1758-59 by Capability Brown.[10] The dining room was vibrantly repainted by the Hare Krishnas in the 1970s-80s.[17]
The central room on the south side is a saloon, probably by Brown and Vassalli. It has an elaborate ceiling, with three panels, deep coving, and a cornice, along with two Ionic fireplaces, and Palladian doorcases.[10] George III was entertained by George Coventry, the 6th Earl, in the house's Saloon.[2] A drawing room is to the west of the saloon, and features rococo plasterwork and a marble fireplace.[10]
To the east of the saloon is the Tapestry Room.[10] This was designed in 1763-71, based on a design by Robert Adam, and contained tapestries and furniture covers possibly designed by Jacques Germain Soufflot, and made by Manufacture Nationale des Gobelins.[23] Around 1902 the ninth Earl sold the tapestries and seating to a Parisian dealer. In 1949 the Samuel H. Kress Foundation purchased the ceiling, floor, mantlepiece, chair rails, doors and the door surrounds, which were donated to the Metropolitan Museum of Art, New York, in 1958. In 1959 the Kress Foundation also helped the Metropolitan Museum acquire the chair and sofa frames, which they recovered using the original tapestry seats.[7][23] A copy of the ceiling was installed in place of the original.[10] As of 2016, the room is displayed as it would have looked after the tapestries had been sold, with a jug and ewer on display as the only original decoration of the room that remains in it. The adjacent library room is used to explain what happened to the tapestry room;[17] the former library was designed by Adam, and was dismantled except for the marble fireplace.[10]
At the west side of the building is a long gallery,[10] which was designed by Robert Adam and installed between 1761 and 1766. It is the best preserved of the original interior (little of the rest has survived in situ).[1] It has an octagonal panelled ceiling, and plaster reliefs of griffins. A half-hexagonal bay faces the garden. The room also contains a marble caryatid fireplace designed by J Wilton.[10] As of 2016, modern sculptures are displayed in empty niches along the Long Gallery
wikipedia
To be completely honest,introducing my newest edition to the family is kinda hard for me.
growing up in a very strict Canon house,the word Nikon should have never even cross my mind,not to mention actually using one,or,god forbidden,owning one.
"and then i saw her standing there..." is pretty much the way to describe it.
she looked like my Canon AE1P younger sister and i was just like......well,fuck it. you only live once.
although she still feels a bit strange to handle (why is everything reversed?!)
im sure we'll have lots of fun times together :)
The Nikon EM was manufactured by Nippon Kogaku K. K. (today Nikon Corporation) in Japan from 1979 to 1982 and uses a Seiko MFC-E focal plane shutter with a speed range of 1 to 1/1000 second plus Bulb and flash X-sync of 1/90 second. The EM has no full manual exposure mode capability and accepts nearly all lenses with the Nikon F bayonet mount.
The Nikon EM formed the base of the new line. It was the smallest and cheapest SLR ever made by Nippon Kogaku. It was a battery-powered (two S76 or A76, or one 1/3N) electromechanically controlled manual focus SLR. The EM featured a lightweight and compact hybrid copper aluminum alloy body and fiberglass reinforced polycarbonate plastic top and bottom covers, plus aperture priority semiautomatic exposure control governed by a built-in 60/40 percent centerweighted, silicon photodiode light meter. A left side viewfinder galvanometer needle pointer indicated the exposure on a shutter speed scale. The viewfinder also had Nikon’s standard 3 mm split image rangefinder and 1 mm microprism collar focusing aids, but the focus screen was fixed. The viewfinder is dimmer than those in the semi-professional Nikons since the expensive prisms of the latter were not used. The camera is also fitted with a low-light exposure warning in the form of an audible 'beep'.
The EM also had one very rare feature for an electronically controlled camera. Nippon Kogaku’s philosophy that a camera must always work when called upon resulted in the EM’s backup ability to operate without batteries – albeit in a limited fashion: completely manual mechanical control with limited shutter speeds (1/90 second, marked M90, or Bulb) and without the light meter. (A little-known feature of the EM is that when the battery is removed, the "Auto" setting produces a shutter speed of approximately 1/1000 sec. This is documented in the factory repair manual.)
SAC02 - Boeing C-17A Globemaster III - NATO Strategic Airlift Capability (in Hungarian Air Force markings)
at Toronto Lester B. Pearson Airport (YYZ)
The Strategic Airlift Capability (SAC) is a consortium of 12 nations, 10 of which are member states of NATO and two of which are Partnership for Peace (PfP) members, to pool resources in order to operate 3 Boeing C-17 Globemaster III aircraft for joint strategic airlift purposes.
The SAC Heavy Airlift Wing is based at Pápa Air Base in Hungary
Member states are NATO members Bulgaria, Estonia, Hungary, Lithuania, the Netherlands, Norway, Poland, Romania, Slovenia and the United States of America, and Partnership for Peace countries Finland and Sweden.
This was taken at the very limit of my camera's capability from the hill above Fintray Bay. The ferry is the one that plies the route between Wemyss Bay and Rothesay.
Broadway Tower is a folly on Broadway Hill, near the village of Broadway, in the English county of Worcestershire, at the second-highest point of the Cotswolds (after Cleeve Hill). Broadway Tower's base is 1,024 feet (312 metres) above sea level. The tower itself stands 65 feet (20 metres) high.
The "Saxon" tower was the brainchild of Capability Brown and designed by James Wyatt in 1794 in the form of a castle, and built for Lady Coventry in 1798–99. The tower was built on a "beacon" hill, where beacons were lit on special occasions. Lady Coventry wondered whether a beacon on this hill could be seen from her house in Worcester — about 22 miles (35 km) away — and sponsored the construction of the folly to find out. Indeed, the beacon could be seen clearly.
Over the years, the tower was home to the printing press of Sir Thomas Phillipps, and served as a country retreat for artists including William Morris and Edward Burne-Jones who rented it together in the 1880s. William Morris was so inspired by Broadway Tower and other ancient buildings that he founded the Society for the Protection of Ancient Buildings in 1877.
Today, the tower is a tourist attraction and the centre of a country park with various exhibitions open to the public at a fee, as well as a gift shop and restaurant. The place is on the Cotswold Way and can be reached by following the Cotswold Way from the A44 road at Fish Hill, or by a steep climb out of Broadway village.
Near the tower is a memorial to the crew of an A.W.38 Whitley bomber that crashed there during a training mission in June 1943.
SAC 01 NATO Strategic Airlift Capability Boeing C-17A Globemaster III - cn F-207 landing @TRD/ENVA 10.03.16
Location: Sherborne New Castle, Sherborne, Dorset, England, UK.
Sherborne New Castle or Sherborne Lodge, as it was originally called, was built by Sir Walter Raleigh in 1594, after the land had been leased to him in 1592 by Queen Elizabeth. There was already an old castle in the grounds but Raleigh elected to build a new property as a temporary home, to entertain his wealthy chums, rather than refurbish the old castle, which is now a ruin.
Raleigh later fell out of favour with the Royals and was carted off to the Tower of London. During Raleigh's imprisonment in the Tower, King James leased the estate to Robert Carr and then sold it to Sir John Digby, 1st Earl of Bristol in 1617.
Digby set about landscaping the gardens and had 'Capability' Brown design and create the lake. The castle has been the Digby family home ever since.
As for Walt, sadly he got the chop in 1618. Allegedly, his last words , whilst his head was on the block, were "strike man strike". Tough cookie or what?
Thank you for visiting - your faves and comments are all very much appreciated.
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A Strategic Airlift Capability/Heavy Airlift Wing Boeing C-17A Globemaster III parked on the apron of Eindhoven Air Base
Harewood House, near Leeds, West Yorkshire
Harewood House is a Grade 1 Country House near Leeds in West Yorkshire.
It was designed by architects John Carr and Robert Adam and built between 1759 and 1771 for wealthy plantation and slave owner Edwin Lascelles - the 1st Baron Harewood, and is still home to the Lascelles family.
The 1000 acre grounds were designed by Capability Brown.
The house is one of the ten 'Treasure Houses of England'.
A spectacular house and grounds that is well worth a visit, but uncomfortable about the source of the wealth that built it.