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It is chilly and rainy in Arizona for Super Bowl 48 but BMW turned up the heat with their all-electric i3 and hybrid i8 sports car. To add additional flavor to the recipe New England Patriots’ starting corner Kyle Arrington and wife VaShonda Arrington joined the experience for the energetic weekend festivities.
Kyle spent a few days in both vehicles during his activities, which included stops at the Nike Football Super Bowl Hospitality Gifting Suite at the immaculate Scottsdale Resort & Conference Center, the NFL Experience, family outings and dinner with his spouse. Vashonda’s centerpiece moment was raising funds for the Off the Field Player’s Wives Association’s “14th Annual Super Bowl Fashion Show” held at the upscale Scottsdale Fashion Mall. The wives, kids and a handful of former NFL players walked the runway with grace and style. Guests included Holly Robinson Peete, Antonio Cromardie, Steve Young, Kevin Hart and many more. She enjoyed the earthly interior of the i3 and spoke passionately about the need regarding increased sustainability in the world.
The mind is driven by thoughts and fueled by inventive answers. The i3 is 100% pure electric and the i8 is a plug-in hybrid sports car, which means its power is sourced from both gasoline and electricity. The i8 is comprised of a Life module and a Drive module. The 3-liter gasoline motor is placed in the rear and the smaller electric engine is housed up front. In addition, the i8 is essentially an AWD vehicle channeling traction from both axles simultaneously but doesn’t utilize the company’s hallmark xDrive system. A few common i8 performance specs include:
•0 to 60 mph = 4.2 seconds
•Top speed = 155 mph (electronically limited)
•Electric only top speed = 75 mph
•Pure electric range = 22 miles
Born electric, the i3 is engineered with BMW’s LifeDrive architecture, which is also structured into two categories, the Life Module and the Drive Module. Comprised of high-strength carbon, the Life Module protects and provides comfort for the driver and passengers. The second platform, the Drive Module, encompasses the electric drive system, the suspension and the HVAC. Since the car is lighter, the liquid-cooled lithium-ion battery (developed in-house by BMW) is smaller and only needs three hours for a full stage-2 (240-volt) charge. Additionally, BMW attempts to use as much renewable energy as possible for the manufacturing process of the carbon fiber i3.
The journey continues towards educating the world on the benefits of going green. BMW is both an innovator and leader in this technology category and has already spearheaded a positive movement. Expect more BMW i products down the line since they have only just begun.
en.wikipedia.org/wiki/De_Havilland_Dove#Variants
en.wikipedia.org/wiki/Yorkshire_Air_Museum#Collection
The de Havilland DH.104 Dove is a British short-haul airliner developed and manufactured by de Havilland. The design, which was a monoplane successor to the pre-war Dragon Rapide biplane, came about from the Brabazon Committee report which, amongst other aircraft types, called for a British-designed short-haul feeder for airlines.
The Dove was a popular aircraft and is considered to be one of Britain's most successful postwar civil designs, with over 500 aircraft manufactured between 1946 and 1967. Several military variants were operated, such as the Devon by the Royal Air Force and the Sea Devon by the Royal Navy, and the type also saw service with a number of overseas military forces.
A longer four-engined development of the Dove, intended for use in the less developed areas of the world, was the Heron. A considerably re-designed three-engined variant of the Dove was built in Australia as the de Havilland Australia DHA-3 Drover.
The development team for the Dove was headed by Ronald Bishop, the creator of the de Havilland Mosquito, a wartime fighter-bomber, and the de Havilland Comet, the first commercial jet aircraft in the world. It had been developed to meet the Type VB requirement issued by the Brabazon Committee. In concept, the Dove was developed to be the replacement of the pre-war Dragon Rapide. It was also required to be competitive with the large numbers of surplus military transports in the aftermath of the Second World War, such as the Douglas DC-3. Unlike the Dragon Rapide, the Dove's structure was entirely metal. It featured innovations including constant-speed propellers, flaps, and a retractable tricycle undercarriage.
In 1946, aviation magazine Flight praised the qualities of the newly developed Dove, noting its "modernity" as well as the aircraft's load-carrying capacity, safe engine-failure performance, and positive maintenance features. Considerable attention was paid to aspects of maintainability, many of the components being designed to be interchangeable and easy to remove or replace, such as the rudder, elevator, and power units; other areas include the mounting of the engines upon four quick-release pickup points, the routing of cables and piping, and the detachable wings and tail cone. The extensive use of special Redux metal-bonding adhesives reduced the need for riveting during the manufacturing process, reducing overall weight and air-skin friction.
While standard passenger versions of the Dove would carry between eight and eleven passengers, the cabin was designed to allow operators to convert between higher and lower density seating configurations. Features such as a single aircraft lavatory and an aft luggage compartment could be removed to provide increased seating. Various specialised models were produced for other roles, such as aerial survey, air ambulance, and flying classroom. A strengthened cabin floor structure was used to enable concentrated freight loads to be carried as well. The Dove could also serve as an executive transport, and in such a configuration it was capable of seating five passengers; the executive model proved to be popular with various overseas customers, particularly those in the United States.
The crew typically consisted of a pilot and radio operator, although rapidly removable dual flight controls could be installed for a second flying crewmember. A combination of large windows and a transparent perspex cabin roof provided a high level of visibility from the cockpit. From a piloting perspective, the Dove was noted for possessing easy flying qualities and mild stall qualities. A TKS anti-icing system was available for the Dove, involving an alcohol-based jelly delivered via porous metal strips embedded on the leading edges of the wings and tail.
The Dove first flew on 25 September 1945. In December 1946, the Dove entered service with Central African Airways. Initial production of the Dove took place at de Havilland's Hatfield factory, but from 1951 the aircraft were built at the company's Broughton facility near Chester. The final example of the type was delivered in 1967. Production of the Dove and its variants totalled 544 aircraft, including two prototypes, 127 military-orientated Devons and 13 Sea Devons.
From 1946, large numbers were sold to scheduled and charter airlines around the world, replacing and supplementing the pre-war designed de Havilland Dragon Rapide and other older designs. The largest order for the Dove was placed by Argentina, which ultimately took delivery of 70 aircraft, the majority of which were used by the Argentine Air Force. LAN Chile took delivery of twelve examples and these were operated from 1949 onwards until the aircraft were sold to several small regional airlines in the United States in 1954.
In excess of 50 Doves were sold to various operators in the United States by Jack Riley, an overseas distributor for the type. De Havilland later assumed direct control of U.S. sales, but did not manage to match this early commercial success for the type.
An early batch of 30 Devons was delivered to the Royal Air Force and they were used as VIP and light transports for over 30 years. The Royal New Zealand Air Force acquired 30 Devons between 1948 and 1954, and these remained in service for VIP, crew-training and light transport duties into the 1970s.
The Biafran Air Force operated a single Dove during the Nigerian Civil War; the aircraft was lost, to be subsequently found in 1970 on the premises of a school in Uli. A second US-registered Riley Dove, N477PM delivered in 1967 to Port Harcourt from Switzerland, never reached Biafra because it was stopped by Algerian authorities.
A few Doves and civilianised Devons remained in use in 2011 in the United Kingdom, Canada, Germany and elsewhere with small commercial firms and with private pilot owners.
The Yorkshire Air Museum & Allied Air Forces Memorial is an aviation museum in Elvington, York on the site of the former RAF Elvington airfield, a Second World War RAF Bomber Command station. The museum was founded, and first opened to the public, in the mid 1980s.
The museum is one of the largest independent air museums in Britain. It is also the only Allied Air Forces Memorial in Europe. The museum is an accredited museum under Arts Council accreditation scheme. It is a Member of Friends of the Few (Battle of Britain Memorial), the Royal Aeronautical Society, the Museums Association and the Association of Independent Museums.
The Museum is a registered charity (No. 516766) dedicated to the history of aviation and was also set up as a Memorial to all allied air forces personnel, particularly those who served in the Royal Air Force during the Second World War.
Site
Further information: RAF Elvington
The 20-acre (81,000 m2) parkland site includes buildings and hangars, some of which are listed. It incorporates a 7-acre (28,000 m2) managed environment area and a DEFRA and Environment Agency supported self sustainability project called "Nature of Flight". The museum is situated next to a 10,000 ft runway, which is privately owned.
History
Whilst the Royal Air Force carried on using the runway for aircraft landing and take off training until 1992, the buildings and hangars had long been abandoned. In 1980 Rachel Semlyen approached the owners of "what was then an abandoned and derelict wartime site, with the idea of restoring the buildings and creating a museum". In 1983, a group started clearing the undergrowth and the site was ready to be unveiled as the Yorkshire Air Museum in 1986.
Events
The Museum undertakes several annual events each year within the general attraction / entertainment area as well as educational / academic events for specific audiences, plus several corporate events in association with companies such as Bentley, Porsche, banking, government agencies etc. The unique annual Allied Air Forces Memorial Day takes place in September.
Exhibits
The Museum has over 50 aircraft spanning the development of aviation from 1853 up to the latest GR4 Tornado. Several aircraft including Victor, Nimrod, Buccaneer, Sea Devon, SE5a, Eastchurch Kitten, DC3 Dakota are kept live and operated on special "Thunder Days" during the year. Over 20 historic vehicles and a Registered Archive containing over 500,000 historic artefacts and documents are also preserved at the Museum, which is also the Official Archive for the National Aircrew Association and National Air Gunners Association. It is nationally registered and accredited through DCMS/Arts Council England and is a registered charity.
A permanent exhibition on RAF Bomber Command was opened at the museum by life member, Sir David Jason. In 2010 a new exhibition called "Pioneers of Aviation", and funded by the Heritage Lottery Fund, was opened featuring the lives and achievements of Sir George Cayley, Sir Barnes Wallis, Robert Blackburn, Nevil Shute and Amy Johnson.
Principal on-site businesses include: Restaurant, Retail Shop, Events, Aircraft Operation Engineering Workshops, Archives and Corporate Business Suite. The museum is also a location for TV and film companies.
Building 1 – Airborne Forces Display & No. 609 Squadron RAF Room
Building 2 – Uniform Display
Building 3 – Air Gunners' Exhibition
Building 4 – Archives & Reference Library
Building 5 – Museum Shop
Building 7 – Memorial Garden
Building 8 – Museum HQ, Main Entrance
Building 9 – Against the Odds
Building 10 – Elvington Corporate Room
Building 11 – Museum NAAFI Restaurant
Building 12 – Control Tower
Building 13 – French Officers' Mess
Building 14 – Airmens Billet and Station MT Display
Building 15 – Royal Observer Corp
Building 16 – Signal Square
Building 17 – Hangar T2 Main Aircraft exhibition
Building 18 – Archive & Collections Building
Building 19 – Handley Page Aircraft Workshop
Building 20 – Pioneer of Aviation Exhibition
Collection
Aircraft on display
Pre-World War II
Avro 504K – Replica
Blackburn Mercury – Replica
Cayley Glider – Replica
Mignet HM.14 Pou-du-Ciel
Port Victoria P.V.8 Eastchurch Kitten Replica
Royal Aircraft Factory BE.2c – Replica
Royal Aircraft Factory SE.5a – Replica
Wright Flyer – Replica
World War II
Avro Anson T.21 VV901
Douglas Dakota IV KN353
Fairchild Argus II FK338
Gloster Meteor F.8 WL168
Gloster Meteor NF.14 WS788
Handley Page Halifax III LV907
Hawker Hurricane I – Replica
Messerschmitt Bf 109 G-6 – Replica
Slingsby T.7 Kirby Cadet RA854
Supermarine Spitfire I – Replica
Waco Hadrian 237123
Post World War II
Air Command Commander Elite
Beagle Terrier 2 TJ704
Canadair CT-133 Silver Star 133417
de Havilland Devon C.2 VP967
de Havilland Vampire T.11 XH278
Europa Prototype 001
Mainair Demon
Saunders-Roe Skeeter AOP.12 XM553
Westland Dragonfly HR.5 WH991
Cold War
BAC Jet Provost T.4 XP640
Blackburn Buccaneer S.2 XN974
Blackburn Buccaneer S.2B XX901
British Aerospace Harrier GR.3 XV748
British Aerospace Nimrod MR.2 XV250
Dassault Mirage IIIE 538
Dassault Mirage IVA 45/BR
English Electric Canberra T.4 WH846
English Electric Lightning F.6 XS903 which arrived during June 1988.
Fairey Gannet AEW.3 XL502
Gloster Javelin FAW.9 XH767
Handley Page Victor K.2 XL231
Hawker Hunter FGA.78 QA10
Hawker Hunter T.7 XL572
Panavia Tornado GR.1 ZA354
Panavia Tornado GR.4 XZ631
Ground vehicles
Second World War
Thompson Brothers Aircraft Refueller
1938 Ford Model E
1940 "Tilly" Standard 12 hp Mkl RAF Utility Vehicle
1941 Chevrolet 4x4 CMP
1942 Austin K2 NAAFI Wagon
1942 Thornycroft ‘Amazon’ Coles Crane
Cold War
1947 Commer one and a half deck airport coach
1949 Citroen 11BL
1948 David Brown VIG.2 Aircraft Tractor
1949 David Brown VIG.3 Aircraft Tractor
1951 David Brown GP Airfield Tractor
1953 Alvis Saracen 12ton APC
1953 Austin Champ Cargo 4x4 General Purpose Vehicle
1956 Green Goddess Self Propelled Pump
1958 Commer Q4 Bikini Fire Pump Unit
1958 Lansing Aircraft Carrier Type Tug
1959 Daimler Ferret ASC MK.2/3/7
1966 Chieftain Main Battle Tank
1970 Douglas P3 nuclear aircraft 25 tonne tug
1971 Pathfinder Fire Engine 35ton (ex. Manchester Airport)
1972 TACR2 Range Rover - 6 wheeled fast response fire unit
1974 GMC 6 wheeled fast response airfield fire truck
1976 Dennis Mercury 17.5 tonne aircraft tug
Pathfinder Fire Engine
Visiting the Redpath sugar factory during Doors Open Toronto. They led us into this room and showed us an occasionally hilarious video on the sugar manufacturing process.
The Sochi 2014 medals are being manufactured by the experts at Adamas, a Sochi 2014 Supplier and Russia’s leading jeweler. Each medal takes up to 18 hours to be created and the latest design and technology processes have been used in the manufacturing process.
Brian Temple, the Europe District Public Affairs chief, delivered his “Science behind the Magic” presentation to several classes May 9 at Aukamm Elementary School in Wiesbaden, Germany. He performed for about 200 students overall. It’s part of the district’s educational outreach program, under which Corps officials share instructional opportunities related to science, technology, engineering and math. The presentation focused on chemistry, mixtures and compounds, along with various manufacturing processes for coins, rope and flash paper. Temple showed slides and videos highlighting each scientific element, then followed it up with a magic trick demonstrating the science and technological aspects of his art. He lit the flash paper on fire and turned it into a $100 bill, drawing gasps and looks of amazement from the students. As an organization, USACE is working to engage students early and be a constant resource throughout their academic development in an effort to promote STEM careers and pursuits. “You have the coolest presentation we see all year,” third-grader Sara Uharriet, 9, told Temple. “It’s just very interesting, and we get to learn a lot of cool things.” (U.S. Army Corps of Engineers photo by Vince Little)
L.L Bean flagship store in Freeport Maine
L.L.Bean was founded in 1912 by avid hunter and fisherman Leon Leonwood Bean—born October 13, 1873, in Greenwood, Maine—who had developed a waterproof boot (a combination of lightweight leather uppers and rubber bottoms) that he sold to hunters. He obtained a list of nonresident Maine hunting license holders, prepared a descriptive mail order circular, set up a shop in his brother's basement in Freeport, Maine, and started a nationwide mail order business. By 1912, he was selling the "Bean boot," or Maine Hunting Shoe, through a four-page mail-order catalog, and the boot remains a staple of the company's outdoorsy image. Defects in the initial design led to 90% of the original production run being returned: Bean made good on his money-back guarantee, corrected the design, and continued selling them. Leon L. Bean died on February 5, 1967, in Pompano Beach, Florida. The company passed into the directorship of Bean's grandson, Leon A. Gorman, from that time until 2001, when Gorman decided to take the position of Chairman of the Board, leaving the position of CEO to Christopher McCormick, the first non-family member to assume the title.[1]
L.L.Bean has a history of high quality manufacturing processes and products as well as excellent customer service. Their return policy is noted as being one of the best for any retailer. It is not uncommon to hear stories of L.L.Bean giving a customer a brand new product after one is brought in for repair.
Lancia Hyena:
Overview:
ManufacturerZagato on Lancia mechanicals
Also calledLancia Delta Zagato Hyena
Production1992–1996
24 made
AssemblyRho, Milan
DesignerMarco Pedracini at Zagato
Body and chassis
ClassSports car
Body style2-door coupé
LayoutTransverse front-engine, four-wheel drive
RelatedLancia Delta Integrale "Evoluzione"
Powertrain
Engine2.0 L I4 (turbocharged petrol)
Transmission5-speed manual
The Lancia Hyena was a 2-door coupé made in small numbers by Italian coachbuilder Zagato on the basis of the Delta HF Integrale "Evoluzione".
History:
The Hyena was born thanks to the initiative of Dutch classic car restorer and collector Paul V.J. Koot, who desired a coupé version of the multiple World Rally Champion HF Integrale. He turned to Zagato, where Hyena was designed in 1990 by Marco Pedracini. A first prototype was introduced at the Brussels Motor Show in January 1992.
Decision was taken to put the Hyena into limited production. Fiat refused to participate in the project supplying bare HF Integrale chassis, which complicated the manufacturing process: the Hyena had to be produced from fully finished HF Integrales, privately purchased at Lancia dealers. Koot's Lusso Service took care of procuring and stripping the donor cars in the Netherlands; they were then sent to Zagato in Milan to have the new body built and for final assembly. All of this made the Hyena very expensive to build and they were sold for around 140,000 Swiss francs or $75,000 (£49,430).
A production run of 75 examples was initially planned, but only 25 Hyenas were completed between 1992 and 1993.
Specifications:
The Zagato bodywork made use of aluminium alloys and composite materials; the interior featured new dashboard, console and door cards made entirely from carbon fibre. Thanks to these weight saving measures the Hyena was some 150 kilograms (330 lb) lighter than the original HF Integrale, about 15% of its overall weight. The two-litre turbo engine was upgraded from 205 to 250 PS (184 kW), and the car could accelerate from 0–100 km in 5.4 seconds.
[Text from Wikipedia]
en.wikipedia.org/wiki/Lancia_Delta#Lancia_Hyena
This miniland-scale Lego Lancia Hyena (1992 - Zagato) has been created for Flickr LUGNuts' 92nd Build Challenge, - "Stuck in the 90's", - all about vehicles from the decade of the 1990s.
It is chilly and rainy in Arizona for Super Bowl 48 but BMW turned up the heat with their all-electric i3 and hybrid i8 sports car. To add additional flavor to the recipe New England Patriots’ starting corner Kyle Arrington and wife VaShonda Arrington joined the experience for the energetic weekend festivities.
Kyle spent a few days in both vehicles during his activities, which included stops at the Nike Football Super Bowl Hospitality Gifting Suite at the immaculate Scottsdale Resort & Conference Center, the NFL Experience, family outings and dinner with his spouse. Vashonda’s centerpiece moment was raising funds for the Off the Field Player’s Wives Association’s “14th Annual Super Bowl Fashion Show” held at the upscale Scottsdale Fashion Mall. The wives, kids and a handful of former NFL players walked the runway with grace and style. Guests included Holly Robinson Peete, Antonio Cromardie, Steve Young, Kevin Hart and many more. She enjoyed the earthly interior of the i3 and spoke passionately about the need regarding increased sustainability in the world.
The mind is driven by thoughts and fueled by inventive answers. The i3 is 100% pure electric and the i8 is a plug-in hybrid sports car, which means its power is sourced from both gasoline and electricity. The i8 is comprised of a Life module and a Drive module. The 3-liter gasoline motor is placed in the rear and the smaller electric engine is housed up front. In addition, the i8 is essentially an AWD vehicle channeling traction from both axles simultaneously but doesn’t utilize the company’s hallmark xDrive system. A few common i8 performance specs include:
•0 to 60 mph = 4.2 seconds
•Top speed = 155 mph (electronically limited)
•Electric only top speed = 75 mph
•Pure electric range = 22 miles
Born electric, the i3 is engineered with BMW’s LifeDrive architecture, which is also structured into two categories, the Life Module and the Drive Module. Comprised of high-strength carbon, the Life Module protects and provides comfort for the driver and passengers. The second platform, the Drive Module, encompasses the electric drive system, the suspension and the HVAC. Since the car is lighter, the liquid-cooled lithium-ion battery (developed in-house by BMW) is smaller and only needs three hours for a full stage-2 (240-volt) charge. Additionally, BMW attempts to use as much renewable energy as possible for the manufacturing process of the carbon fiber i3.
The journey continues towards educating the world on the benefits of going green. BMW is both an innovator and leader in this technology category and has already spearheaded a positive movement. Expect more BMW i products down the line since they have only just begun.
In the heart of Old Town, historic factory is among the oldest in Grasse ... Indeed the current premises sheltered from their beginning in 1782, a perfume factory. In 1926, after the famous painter Jean Honoré Fragonard, it takes the name of Parfumerie Fragonard. Since then, every day, we produce are our perfumes, cosmetics and soaps in a respectful environment of tradition. We would be happy to welcome you and offer you a guided tour during which you will discover the different manufacturing processes and packaging our products. At the end of your visit, you can admire 3000 years of history of perfume through our private museum.
Dedicated to the perfume and aromatic plants, Flower Factory is surrounded by a beautiful garden scented plants ... the gates of Grasse, this contemporary factory opened in 1986 is equipped with very modern machinery for the manufacture and packaging of our products.
WORKSHOP ODOR "Perfumer's Apprentice"
Available on the French Riviera and Paris, in factories, workshops Perfumers Apprentice can discover the expertise of Perfumer: the history of perfume, raw materials and different extraction methods.
Experience unforgettable sense centered on the composition of a toilet water (100 ml) in aromatic notes of citrus and orange blossom, by assembling the different species made available. A fun and exciting experience in the world of perfumery, which proposes the course led by the teacher, the bottle and its bag, apron "apprentice" printed Fragonard, the diploma signed by the teacher and the summary of the composition .
One of our guides will accompany you as a result of the workshop for a visit "Prestige" from our factory.
Located in one of the oldest houses in the historic center of the city, this perfume offers original creations of Didier Gaglewski.
Didier Gaglewski, "nose" in Grasse, began offering its achievements in the framework Living in Provence and in Paris, Germany and Switzerland. Both "artisan", "artist", he decided to offer his achievements directly driven by the idea that the quality, originality and respect perfume composition will dress with fun, humor and quality its customers.
Requiring each of its perfumes, made in the privacy of his laboratory, took several months of research. In partnership with Michelle Cavalier and the "garden of La Bastide," Didier Gaglewski also remains closer to the flowers and working the land. Try to trace extraction techniques inherited from the past and plants specific to the region perfumes seduce and make a very personal and authentic. This atypical creator is distinguished by its compositions made in Grasse basin, its choice to favor natural raw materials and the search for sobriety.
Front satisfaction and customer demands wishing to regain the proposed perfumes, shop in Grasse, 12 rue of the Oratory, just steps from the International Perfume Museum to discover the scents and recent creations.
The country house of Aromas
Based in Saint Cézaire on Siagne in the Pays de Grasse, the Bastide aromas manufactures and packages fragrances since 1995.
Saint Cézaire on Siagne is a typical Provencal village a few kilometers from Grasse, the world capital of perfumery.
The homemade studio human scale can meet all your demands. The 100% handmade is carried out in the workshop without intermediary, under the control of a chemist.
La Bastide des Aromas, respects the traditions of the Grasse region and offers the exclusive fragrances custom made in the workshop on-site, high quality, with particular stress on the fragrance concentration, her outfit and originality.
David Mellor Visitor Centre
David Mellor is internationally famous for his cutlery.
His chic factory in Hathersage, designed by Sir Michael Hopkins, and purpose-built on the site of the old gasworks, is hailed as a minor masterpiece of modern architecture.
Built in local gritstone with a spectacular lead roof, it blends beautifully into the rural landscape. The factory is open for viewing on Sundays and visitors are welcome to take a look around and watch the various designs being made.
The manufacturing process is surprisingly low-tech and most of it done by hand – if nothing else this explains why the cutlery is so expensive (and so collectable).
In addition to the factory, there is also a stylish shop, a classy café and an interesting design museum.
David Mellor died in 2009, and his talented son Corin continues the design tradition at Hathersage.
Café
My image shows the classy café.
Production Type; Just in time manufacture!
Imagine my amazement on accompanying a bride to a prestigious salon in Lahore, far from the intimate environment one may expect my friend was one of 137 brides beautified and prepped to be wed that day alone!! This was not to mention each bride was accompanied by a bridal party also in need of 'party makeover'!
I was amused and amazed by the intense atmosphere of 100+ nervous brides and the military efficiency of the beauticians and stylist. Weddings are a big deal in Pakistan and I defiantly got caught up in the full swing of bridal season.
Each bride had an itinerary and check list, they entered looking quiet plain in one location and were directed through various stops. Completion of each station (post) allowed them to tick off an item of their list: cleansing stn, foundation stn, Nails, etc etc.... finally (several hours later) a bride emerges.
This may explain the title bridal factory, it reminded me of a conveyor belt on 'How's it made' with various stages in the manufacturing process of a bride / dulhan, with a well oiled & co-ordinated team.
As I left I remarked to a young tired looking hair stylist " Well at least it's Sunday tomorrow, I'm sure you can put your feet up". She managed half a smile and replied "Not likely baji (sister), we have another 152 brides booked in".
This picture shows three brides awaiting the final stage in their preparation, the silk scarfs are placed in position and secured, not dissimilar to the white veil a western bride would wear...well perhaps somewhat heavier.
In the heart of Old Town, historic factory is among the oldest in Grasse ... Indeed the current premises sheltered from their beginning in 1782, a perfume factory. In 1926, after the famous painter Jean Honoré Fragonard, it takes the name of Parfumerie Fragonard. Since then, every day, we produce are our perfumes, cosmetics and soaps in a respectful environment of tradition. We would be happy to welcome you and offer you a guided tour during which you will discover the different manufacturing processes and packaging our products. At the end of your visit, you can admire 3000 years of history of perfume through our private museum.
Dedicated to the perfume and aromatic plants, Flower Factory is surrounded by a beautiful garden scented plants ... the gates of Grasse, this contemporary factory opened in 1986 is equipped with very modern machinery for the manufacture and packaging of our products.
WORKSHOP ODOR "Perfumer's Apprentice"
Available on the French Riviera and Paris, in factories, workshops Perfumers Apprentice can discover the expertise of Perfumer: the history of perfume, raw materials and different extraction methods.
Experience unforgettable sense centered on the composition of a toilet water (100 ml) in aromatic notes of citrus and orange blossom, by assembling the different species made available. A fun and exciting experience in the world of perfumery, which proposes the course led by the teacher, the bottle and its bag, apron "apprentice" printed Fragonard, the diploma signed by the teacher and the summary of the composition .
One of our guides will accompany you as a result of the workshop for a visit "Prestige" from our factory.
Located in one of the oldest houses in the historic center of the city, this perfume offers original creations of Didier Gaglewski.
Didier Gaglewski, "nose" in Grasse, began offering its achievements in the framework Living in Provence and in Paris, Germany and Switzerland. Both "artisan", "artist", he decided to offer his achievements directly driven by the idea that the quality, originality and respect perfume composition will dress with fun, humor and quality its customers.
Requiring each of its perfumes, made in the privacy of his laboratory, took several months of research. In partnership with Michelle Cavalier and the "garden of La Bastide," Didier Gaglewski also remains closer to the flowers and working the land. Try to trace extraction techniques inherited from the past and plants specific to the region perfumes seduce and make a very personal and authentic. This atypical creator is distinguished by its compositions made in Grasse basin, its choice to favor natural raw materials and the search for sobriety.
Front satisfaction and customer demands wishing to regain the proposed perfumes, shop in Grasse, 12 rue of the Oratory, just steps from the International Perfume Museum to discover the scents and recent creations.
The country house of Aromas
Based in Saint Cézaire on Siagne in the Pays de Grasse, the Bastide aromas manufactures and packages fragrances since 1995.
Saint Cézaire on Siagne is a typical Provencal village a few kilometers from Grasse, the world capital of perfumery.
The homemade studio human scale can meet all your demands. The 100% handmade is carried out in the workshop without intermediary, under the control of a chemist.
La Bastide des Aromas, respects the traditions of the Grasse region and offers the exclusive fragrances custom made in the workshop on-site, high quality, with particular stress on the fragrance concentration, her outfit and originality.
In the heart of Old Town, historic factory is among the oldest in Grasse ... Indeed the current premises sheltered from their beginning in 1782, a perfume factory. In 1926, after the famous painter Jean Honoré Fragonard, it takes the name of Parfumerie Fragonard. Since then, every day, we produce are our perfumes, cosmetics and soaps in a respectful environment of tradition. We would be happy to welcome you and offer you a guided tour during which you will discover the different manufacturing processes and packaging our products. At the end of your visit, you can admire 3000 years of history of perfume through our private museum.
Dedicated to the perfume and aromatic plants, Flower Factory is surrounded by a beautiful garden scented plants ... the gates of Grasse, this contemporary factory opened in 1986 is equipped with very modern machinery for the manufacture and packaging of our products.
WORKSHOP ODOR "Perfumer's Apprentice"
Available on the French Riviera and Paris, in factories, workshops Perfumers Apprentice can discover the expertise of Perfumer: the history of perfume, raw materials and different extraction methods.
Experience unforgettable sense centered on the composition of a toilet water (100 ml) in aromatic notes of citrus and orange blossom, by assembling the different species made available. A fun and exciting experience in the world of perfumery, which proposes the course led by the teacher, the bottle and its bag, apron "apprentice" printed Fragonard, the diploma signed by the teacher and the summary of the composition .
One of our guides will accompany you as a result of the workshop for a visit "Prestige" from our factory.
Located in one of the oldest houses in the historic center of the city, this perfume offers original creations of Didier Gaglewski.
Didier Gaglewski, "nose" in Grasse, began offering its achievements in the framework Living in Provence and in Paris, Germany and Switzerland. Both "artisan", "artist", he decided to offer his achievements directly driven by the idea that the quality, originality and respect perfume composition will dress with fun, humor and quality its customers.
Requiring each of its perfumes, made ââin the privacy of his laboratory, took several months of research. In partnership with Michelle Cavalier and the "garden of La Bastide," Didier Gaglewski also remains closer to the flowers and working the land. Try to trace extraction techniques inherited from the past and plants specific to the region perfumes seduce and make a very personal and authentic. This atypical creator is distinguished by its compositions made ââin Grasse basin, its choice to favor natural raw materials and the search for sobriety.
Front satisfaction and customer demands wishing to regain the proposed perfumes, shop in Grasse, 12 rue of the Oratory, just steps from the International Perfume Museum to discover the scents and recent creations.
The country house of Aromas
Based in Saint Cézaire on Siagne in the Pays de Grasse, the Bastide aromas manufactures and packages fragrances since 1995.
Saint Cézaire on Siagne is a typical Provencal village a few kilometers from Grasse, the world capital of perfumery.
The homemade studio human scale can meet all your demands. The 100% handmade is carried out in the workshop without intermediary, under the control of a chemist.
La Bastide des Aromas, respects the traditions of the Grasse region and offers the exclusive fragrances custom made in the workshop on-site, high quality, with particular stress on the fragrance concentration, her outfit and originality.
Io Aircraft - www.ioaircraft.com
Drew Blair
www.linkedin.com/in/drew-b-25485312/
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
Early preview (Iteration 2) of an entirely new type of aircraft, no info is on the net yet and won't be for a while. RANGER - 2 Passenger VTOL Hypersonic Plane
Drew Blair
www.linkedin.com/in/drew-b-25485312/
Vertical take off and landing - High Supersonic into Hypersonic Realm. Economy cruise above Mach 4, and can accelerate to beyond Mach 8. Non VTOL, could reach LEO. With a range of 5,000+ nm (8,000-10,000nm non vtol). Fuel H2, reducing fuel weight 95%.
Length, 35ft (10.67m), span 18ft (6m).
Propulsion, 2 Unified Turbine Based Combined Cycle. 2 Unified thrust producing gas turbine generators that provide the power for the central lifting fan (electric, not shaft driven) and the rear VTOL.
Estimated market price, $25-$30 million in production. New York to Dubai in an hour.
All based on my own technology advances in Hypersonics which make Lockheed and Boeing look ancient.
-------------
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
After 3 months of travel, which included approximately 7 weeks of sitting at Osaka International Airport, my Mandarake purchase in April 2020 finally arrived.
Here she is in all her glory, Sailor Pluto, the last of the Sailor Senshi on my "to get list".
BFF to Chibi-Usa, Sailor Pluto, or "Pu" is the Guardian of Time and leader of the Outer Senshi, soldiers gifted with stronger power than their Inner Senshi cohorts. She is generally stationed at that one spot preventing trespassers from entering the future. Well, things got screwy and required Pluto to not only abandon her post, but eventually abandon her timeline completely and return to the present under the civilian guise of Setsuna Meioh.
In addition to being a very competent soldier, Sailor Pluto also bears one of the three Sacred Talisman, along with Sailor Uranus and Pluto, that are needed to find the Holy Grail, the only thing that can stop "The Silence", the big baddie in Season 3 of the original run.
Plus she's the only one with no sleeves on her tunic, so you KNOW she's badass.
Based on what I was reading, Pluto was a bit annoying to get due to her Exclusive release nature, something that I've run into with several of the Endgame releases.. hence my resorting to Mandarake.
Contents of the box are what you'd expect it to be - the figure, four total face plates (neutral, smiling, shouting, eyes closed), her weapon (Garnet Rod), various hands, and the standard base. The head of the staff comes off just like in the show so you can display Pluto holding her talisman.
While I wish I could say that this was just a copy and paste overview from the other Senshi, there are a few critical items worth noting.
First off, on the positive side of things, to my eyes Sailor Pluto is one of a handful of Sailor Moon Figuarts that got the proportions right, with the other two being Super Sailor Moon and Sailor Saturn. I'm not perfectly confident about her scaling, but that's another story.
Much like the other two, Sailor Pluto's faceplates seem to be the right shape, and actually wrap around her to her neck without any unsightly gaps around the ears.
Now that we got that out of the way, lets talk about the greatest barrier to enjoying this figure - her hair. Sailor Pluto has lovely knee length Olive green hair. Good news, Tamashii Nations replicated this. Bad news, it's one solid piece of hard plastic with one point of articulation on the top of her head which is much more annoying to position than you'd think. The same stiff plastic makes up the front of her hair as well, so overall Pluto has a slightly different sheen to her hair as compared to the other Senshi. Detailing on the hair is average - it won't impress, but it won't make you question the manufacturing process either.
There are a few more exciting poses you can get her into, but in general Pluto is going to be one of those figures that does a lot of epic standing, and even then you might want to consider using the stand full time.
Articulation wise, she's got what the ladies do (ankles, knees, hips with pull down, mid torso, shoulders with some collapse and bicep swivel, elbows, wrists, and head), but as stated above your limiting factor is going to be the hair. I guess if it is any consolation, I don't remember Pluto doing much other than her projectile attacks so no crazy gymnastics come to mind.
Paint work is the usual mix of good and meh when it comes to this line, with the messiest spots around her waist where the white paint meets the skirt - interesting thing to note is that the skirt is a separate piece, so basically this is not a masking issue.. they just really sucked at applying the paint. That's kind of the story overall - it's pretty good, then you hit a spot where you go "OOF". Decals on the face are pretty solid.
Finally there's build quality and yeah, good all around. If you've handled one Senshi you've generally handled them all. In the event you haven't, expect limbs to the right size, joints to be tight, and finishes on the various parts to range from "great" to "you really didn't try that hard did you", a common problem with earlier Figuarts. Overall, most handling will be find though as always extra caution when changing hands or doing any sudden movements is recommended.
That, friends, was the last Sailor Senshi. Pluto looks great as far as aesthetics go, but from an articulation perspective sadly the hair is quite limiting. Still, there's no doubt that Pluto will look great standing in with the rest of the crew, which is probably the only reason you'd be getting one of these to begin with.
Lancia Hyena:
Overview:
ManufacturerZagato on Lancia mechanicals
Also calledLancia Delta Zagato Hyena
Production1992–1996
24 made
AssemblyRho, Milan
DesignerMarco Pedracini at Zagato
Body and chassis
ClassSports car
Body style2-door coupé
LayoutTransverse front-engine, four-wheel drive
RelatedLancia Delta Integrale "Evoluzione"
Powertrain
Engine2.0 L I4 (turbocharged petrol)
Transmission5-speed manual
The Lancia Hyena was a 2-door coupé made in small numbers by Italian coachbuilder Zagato on the basis of the Delta HF Integrale "Evoluzione".
History:
The Hyena was born thanks to the initiative of Dutch classic car restorer and collector Paul V.J. Koot, who desired a coupé version of the multiple World Rally Champion HF Integrale. He turned to Zagato, where Hyena was designed in 1990 by Marco Pedracini. A first prototype was introduced at the Brussels Motor Show in January 1992.
Decision was taken to put the Hyena into limited production. Fiat refused to participate in the project supplying bare HF Integrale chassis, which complicated the manufacturing process: the Hyena had to be produced from fully finished HF Integrales, privately purchased at Lancia dealers. Koot's Lusso Service took care of procuring and stripping the donor cars in the Netherlands; they were then sent to Zagato in Milan to have the new body built and for final assembly. All of this made the Hyena very expensive to build and they were sold for around 140,000 Swiss francs or $75,000 (£49,430).
A production run of 75 examples was initially planned, but only 25 Hyenas were completed between 1992 and 1993.
Specifications:
The Zagato bodywork made use of aluminium alloys and composite materials; the interior featured new dashboard, console and door cards made entirely from carbon fibre. Thanks to these weight saving measures the Hyena was some 150 kilograms (330 lb) lighter than the original HF Integrale, about 15% of its overall weight. The two-litre turbo engine was upgraded from 205 to 250 PS (184 kW), and the car could accelerate from 0–100 km in 5.4 seconds.
[Text from Wikipedia]
en.wikipedia.org/wiki/Lancia_Delta#Lancia_Hyena
This miniland-scale Lego Lancia Hyena (1992 - Zagato) has been created for Flickr LUGNuts' 92nd Build Challenge, - "Stuck in the 90's", - all about vehicles from the decade of the 1990s.
In the heart of Old Town, historic factory is among the oldest in Grasse ... Indeed the current premises sheltered from their beginning in 1782, a perfume factory. In 1926, after the famous painter Jean Honoré Fragonard, it takes the name of Parfumerie Fragonard. Since then, every day, we produce are our perfumes, cosmetics and soaps in a respectful environment of tradition. We would be happy to welcome you and offer you a guided tour during which you will discover the different manufacturing processes and packaging our products. At the end of your visit, you can admire 3000 years of history of perfume through our private museum.
Dedicated to the perfume and aromatic plants, Flower Factory is surrounded by a beautiful garden scented plants ... the gates of Grasse, this contemporary factory opened in 1986 is equipped with very modern machinery for the manufacture and packaging of our products.
WORKSHOP ODOR "Perfumer's Apprentice"
Available on the French Riviera and Paris, in factories, workshops Perfumers Apprentice can discover the expertise of Perfumer: the history of perfume, raw materials and different extraction methods.
Experience unforgettable sense centered on the composition of a toilet water (100 ml) in aromatic notes of citrus and orange blossom, by assembling the different species made available. A fun and exciting experience in the world of perfumery, which proposes the course led by the teacher, the bottle and its bag, apron "apprentice" printed Fragonard, the diploma signed by the teacher and the summary of the composition .
One of our guides will accompany you as a result of the workshop for a visit "Prestige" from our factory.
Located in one of the oldest houses in the historic center of the city, this perfume offers original creations of Didier Gaglewski.
Didier Gaglewski, "nose" in Grasse, began offering its achievements in the framework Living in Provence and in Paris, Germany and Switzerland. Both "artisan", "artist", he decided to offer his achievements directly driven by the idea that the quality, originality and respect perfume composition will dress with fun, humor and quality its customers.
Requiring each of its perfumes, made in the privacy of his laboratory, took several months of research. In partnership with Michelle Cavalier and the "garden of La Bastide," Didier Gaglewski also remains closer to the flowers and working the land. Try to trace extraction techniques inherited from the past and plants specific to the region perfumes seduce and make a very personal and authentic. This atypical creator is distinguished by its compositions made in Grasse basin, its choice to favor natural raw materials and the search for sobriety.
Front satisfaction and customer demands wishing to regain the proposed perfumes, shop in Grasse, 12 rue of the Oratory, just steps from the International Perfume Museum to discover the scents and recent creations.
The country house of Aromas
Based in Saint Cézaire on Siagne in the Pays de Grasse, the Bastide aromas manufactures and packages fragrances since 1995.
Saint Cézaire on Siagne is a typical Provencal village a few kilometers from Grasse, the world capital of perfumery.
The homemade studio human scale can meet all your demands. The 100% handmade is carried out in the workshop without intermediary, under the control of a chemist.
La Bastide des Aromas, respects the traditions of the Grasse region and offers the exclusive fragrances custom made in the workshop on-site, high quality, with particular stress on the fragrance concentration, her outfit and originality.
iPlay V1
Our design had to be cheap to manufacture, with minimal manufacture processes and a low overall cost. Keeping this in mind I sketched my basic idea and then rendered it. After exporting the DXF files I lasercut them and had my first prototype.
There is an everlasting debate amongst gamers as to which console and controller is the best. I found that the PS3 controller was the most popular second being Xbox 360. The PS3 controller is symettrical unlike the Xbox controller and is so ergonomoic you can often forget you are holding it.
I illustrated the PS3 controller outline to kickstart the CAD process. My design consists of 3 layers of 5mm acrylic creating an iphone cavity depth of 10mm (iPhone 4 has a thickness of 9.3mm) and an overall thickness of 15mm. The structure would be held together with tight fit acrylic rods. I need to carry out test pieces on 2.99+-0.1mm radii to decide what are the best dimensions to use for these slots bearing in mind the lasercutter burns away material.
The whole in the bottom layer is so the device can be pushed out from the case after use.
V2
I asked some students to test the V1 prototype. They liked the product especially its simplicity. There were points that I could develop and improve.
Not all iPhone games auto orientate, hence it was essential I adapted my design so the phone could be rotated 180 degress. This would be easy by simply duplicating the button slots.
In addition to this there was no camera hole. If I were to introduce a camera holeto the design it would have to be duplicated 180 degrees to ensure photos could be taken no matter what orientation the iPhone was.
Taking this on board I designed and manufactured iPlay V2. Although acrylic rod would create a tight fit, 4 drops of dichloromethane would chemically weld the components together for a long lasting permanent fit. After this I used a buffing wheel to create round edges making the product more ergonomic to hold.
V3
Once again I asked some students for feedback on my prototype. They were impressed with how I addressed the previous issues. The only negative point raised was that it would not fit in your pocket. This was the next challenge I faced.
I considered hinging the lower two arms and making them lock into the back of the case. However this would make the design more complex and increase cost and manufacturing processes.
I moved the top pair of holes further up to better distribute the stress. I decided to split the product in half. My V3 model has alternating layers this creates cavities that allow it to be locked together together when not in use as photographed. This would easily fit in you pocket.
The problem the alternating layers created is a less ergonomic shape. Secondly there was nothing holding the two half together when placed on the phone.
In my V4 model I introduced a rubber band which kept the two half together when on the phone. It would also prevent one half form being lost. This created a new problem; the top half of the rubber band would not always line up as there was nothing guiding it. This was my next problem to solve.
V4
My final model would be made from acrylic but I was not going to buff it as that would add a manufacture process and would siginificanty increase the manufacture time. Since I was already using the laser cutter for cutting my components I thought I may aswell engrave some sort of graphics onto the top layer. I decided to remove the gaps in between the layers to make it better to hold and to remodel the rubberband tracks.
V5
I solved the problem of the inconvenient rubber band with two more locating rods on the top. These extra rods would keep the rubber band guided along the correct track. I made a MDF prototype to test my idea and it worked successfully even with coffee stirrers replicating the acrylic rod.
Satisfied with my idea I finally created an acrylic version. This required a bit more thought than previously as I had to accomodate for the thick rubber band. I decided to use 3mm acrylic instead of 5mm to create a thinner profile. This meant I needed a total of 5 layers to accomodate an iPhone 4.
Since I was already using a lasercutter and I wanted the product to appeal to gamers I decided to engrave some patterns. I was going to use a translucent coloured acrylic for the bottom layer and adjust the design so that it covers the camera and flash. This way the case will act as a camera filter and the flash/torch will produce coloured light.
Now that the product was split into halfs the individual components were so small that cutting a single iPlay V5 uses less than an A4 sized amount of 3mm acrylic (the 2D Design screenshot has an A3 page layout). This also meant that it would fit both an iPhone 4 & 5 as the rubber can stretch to accomodate for an iPhone 5. Apart from the height of the iPhone 5 the dimensions are very similair to those of the 4.
I am very pleased with the final product and getting through to the next stage with KFDS. If I were to develop the product further I would find a way to lock the two halves together when not on the phone. This could be done like a jigsaw puzzle or by manipulating the rods into a dowel joint.
As part of the required course knowledge pupils need to be able to outline the process involved in taking a square wooden blank and preparing it for turning between centres. These pictures depict that process chronologically.
Stage 1 * Preparation of wooden blank. Cut to size. Sand square. Mark across diagonals. Centre punch the centre point. Use spring dividers to mark circumference. Repeat on other end.
Stage 2 * Plane off corners down to circumference line. This takes cross section from square to octagon. This reduces force on cutting toll in initial prep of blank. Mount between fork [driven] centre and dead [or live ] centre at tailstock end. Apply grease a dead centre end. apply force from tailstock end to force fork into material at driven end. Adjust toolstock height to suit. Check for clearance.
Stage 3 * Roughout using scraper to diameter. Use combination of gouges and skew chisels to add beads and other decorative detailing as required. Ensure spindle speed is appropriate for material and cross section under consideration. Obey all safety instructions.
A specialist centre to develop new manufacturing processes for lightweight materials for the aerospace and automotive industries is to be set up as a first step towards creating a National Manufacturing Institute for Scotland.
The First Minister announced today that the £8.9m Lightweight Manufacturing Centre, being set up in the former Doosan Babcock facility in Westway, Renfrew, will support highly skilled jobs and help place Scotland at the forefront of lightweight manufacturing.
It is chilly and rainy in Arizona for Super Bowl 48 but BMW turned up the heat with their all-electric i3 and hybrid i8 sports car. To add additional flavor to the recipe New England Patriots’ starting corner Kyle Arrington and wife VaShonda Arrington joined the experience for the energetic weekend festivities.
Kyle spent a few days in both vehicles during his activities, which included stops at the Nike Football Super Bowl Hospitality Gifting Suite at the immaculate Scottsdale Resort & Conference Center, the NFL Experience, family outings and dinner with his spouse. Vashonda’s centerpiece moment was raising funds for the Off the Field Player’s Wives Association’s “14th Annual Super Bowl Fashion Show” held at the upscale Scottsdale Fashion Mall. The wives, kids and a handful of former NFL players walked the runway with grace and style. Guests included Holly Robinson Peete, Antonio Cromardie, Steve Young, Kevin Hart and many more. She enjoyed the earthly interior of the i3 and spoke passionately about the need regarding increased sustainability in the world.
The mind is driven by thoughts and fueled by inventive answers. The i3 is 100% pure electric and the i8 is a plug-in hybrid sports car, which means its power is sourced from both gasoline and electricity. The i8 is comprised of a Life module and a Drive module. The 3-liter gasoline motor is placed in the rear and the smaller electric engine is housed up front. In addition, the i8 is essentially an AWD vehicle channeling traction from both axles simultaneously but doesn’t utilize the company’s hallmark xDrive system. A few common i8 performance specs include:
•0 to 60 mph = 4.2 seconds
•Top speed = 155 mph (electronically limited)
•Electric only top speed = 75 mph
•Pure electric range = 22 miles
Born electric, the i3 is engineered with BMW’s LifeDrive architecture, which is also structured into two categories, the Life Module and the Drive Module. Comprised of high-strength carbon, the Life Module protects and provides comfort for the driver and passengers. The second platform, the Drive Module, encompasses the electric drive system, the suspension and the HVAC. Since the car is lighter, the liquid-cooled lithium-ion battery (developed in-house by BMW) is smaller and only needs three hours for a full stage-2 (240-volt) charge. Additionally, BMW attempts to use as much renewable energy as possible for the manufacturing process of the carbon fiber i3.
The journey continues towards educating the world on the benefits of going green. BMW is both an innovator and leader in this technology category and has already spearheaded a positive movement. Expect more BMW i products down the line since they have only just begun.
Mach 10 Hypersonic Plane - Turbine Based Combined Cycle - IO Aircraft
Drew Blair
www.linkedin.com/in/drew-b-25485312/
20 Passengers plus 3 crew
10,000 mile range
Mach 10 Cruise
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Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
Unified Turbine Based Combined Cycle (U-TBCC) Turbine + Scramjet Engine - IO Aircraft - Drew Blair
www.ioaircraft.com/hypersonic/ranger.php
Drew Blair
www.linkedin.com/in/drew-b-25485312/
Unified Turbine Based Combined Cycle. Current technologies and what Lockheed is trying to force on the Dept of Defense, for that low speed Mach 5 plane DOD gave them $1 billion to build and would disintegrate above Mach 5, is TBCC. 2 separate propulsion systems in the same airframe, which requires TWICE the airframe space to use.
Unified Turbine Based Combined Cycle is 1 propulsion system cutting that airframe deficit in half, and also able to operate above Mach 10 up to Mach 15 in atmosphere, and a simple nozzle modification allows for outside atmosphere rocket mode, ie orbital capable.
Additionally, Reaction Engines maximum air breather mode is Mach 4.5, above that it will explode in flight from internal pressures are too high to operate. Thus, must switch to non air breather rocket mode to operate in atmosphere in hypersonic velocities. Which as a result, makes it not feasible for anything practical. It also takes an immense amount of fuel to function.
-------------
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Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
The Chancellor Rishi Sunak visits Pall Corporation, a biotech business in Ilfracombe north Devon, where he met staff and toured the manufacturing process
From Barfoot's series of coloured lithographs of 1840 depicting the cotton manufacturing process.
Original text written to accompany Lithograph No.1:
"COTTON is a soft downy substance, which is found growing upon trees and plants, that differ from each other in size, as much as the apple tree, differs from the currant-bush; and the pods are closely filled with this soft substance, which surrounds the seeds or pippins, from which other cotton-plants are raised. The stormy winds may carry them to a distance, or they may fall at the foot of the tree, on which they grew, and become new plants of the same kind. The Cotton, which is the fruit of the tree, consisting of fibres like fine hairs, is nearly white, and looks very beautiful. You see before you the picture of a cotton-field, where the seeds have been sown; the plants have grown up, and borne their pretty blossoms, and much of the bloom has turned into fruit, ready to be gathered. The negroes are busy picking the Cotton from the open pods, and placing it in their bags and baskets; and the master is watching and giving them directions. Men soon found out that Cotton was very useful for clothing, and that some kinds were of more value than others, because the fibres are longer, or finer, and better to work; so they take care to cultivate these sorts in countries where they will grow, such as India, Africa, and the warm parts of America. It is always gathered when the weather is dry and fine, and great care is taken to prevent its being spoiled by the sun or rain. We ought to be kind to these poor black people whose labours yield us so many comforts. And ever grateful to the great and good God who has thus caused the earth to produce such good things for our use. Let us praise him, by singing this pretty verse of Dr. Watts.:
There's not a plant or flower below,
But makes thy glory known
And clouds arise, and tempests blow,
By order from the throne."
New Building on the MDIBL campus designed and built to accommodate the growing number of researchers flocking to the site each year uses Hunter Panels for green roof.
Roof Installer: Roof Systems, Main
July 2008: The new, 18,000-square-foot building officially opened
2009: Awarded "Gold" LEED Building Certification
Roof Details:
Roof Systems used 7,800 square feet of Hunter’s insulation products to the 8,700-square-foot shingled portion of the building’s roof. They began by laying down a four-inch layer of standard polyiso over top of the lab’s 22-gauge steel roof deck. Next they installed a four and one half inch layer of Hunter’s innovative H-Shield-NB, staggering the seams from the first layer to reduce thermal bridging and further increase the rooftop’s overall energy efficiency. Consisting of a four-inch layer of polyiso laminated to a heavy-duty, 5/8-inch piece of oriented strand board, H-Shield-NB eliminates the need to install an additional nailer on top of the insulation before attaching the finished roofing material.
Hunter’s four-inch polyiso provides an R-value of 25, while the four and one half inch H-Shield-NB offers an additional R-value of 25.6. Combined, the two layers of insulation created a rooftop with an R-value of over 50, more than enough to help the laboratory reduce its heating and cooling costs.
Besides energy efficiency, Hunter’s polyiso also features other properties that make it good for the environment and good for the lab. The H-Shield NB used for this project featured OSB that was certified by the Forest Stewardship Council (FSC), a non-profit organization devoted to encouraging responsible management of the world’s forests. Lumber with the FSC label, such as the OSB used on the laboratory’s rooftop, was harvested in a sustainable manner with little impact on the environment.
Other sustainable attributes of Hunter’s polyiso include a manufacturing process that features zero ozone depleting potential (ODP), is CFC-free and meets all applicable EPA standards. Hunter’s polyiso also features an FM Class 1 uplift rating and UL Class A fire rating, resulting in a rooftop that provides superior protection against anything Mother Nature has to offer.
In order to fasten the insulation to the rooftop, Roof Systems utilized specialized 10-inch fasteners developed specifically for use with Hunter’s H-Shield-NB, Cool-Vent™ and Cool-Vent II. The fasteners offer increased pullout resistance and are FM approved. They do not require the use of washers or fastener plates, which reduces costs and speeds up installation. The 10-inch screws were installed through the H-Shield-NB and standard polyiso and attached to the building’s metal decking.
After all of the insulation was fastened to the deck, Roof Systems installed a layer of ice and water shield over the entire roof surface and then covered it with a 50-year asphalt shingle. They completed the roof installation by installing a 24-gauge, white, Kynar-coated flashing material that provides a long-term finish and increases the sustainability of the entire project.
View full article and details in Environmental Design & Construction- a web exclusive: www.edcmag.com/Articles/Web_Exclusive/BNP_GUID_9-5-2006_A...
Want more: visit us at www.hpanels.com/
Part of modding your car is making it look good, and looks weren't really a concern when the engineers were designing your ride. It's easy to see that when you open up the hood and it easily looks like a rat's nest. Password knows that looks on the outside don't mean squat if you can't show off what's under the hood. The Password:JDM dry carbon fiber fuse box over-cover for the 2013+ Subaru BRZ / Scion FR-S adheres to your stock fuse box cover and will help clean up the look of your engine bay making your engine stand out, while adding a much needed accent to the scene. Like all of our dry carbon fiber parts that we manufacture, this piece has been precision crafted for a perfect fit and requires no tools or modifications to install. We also use a fade-resistant resin during the manufacturing process which ensures that the part will look as fresh as it did and function as well as the day you bought it.
Note:The Password:JDM Dry Carbon Fiber Fuse Box Over Cover fits over the factory part and is adhered with double side tape.
Features include:
- Perfect dry carbon fitment with structural integrity
- high-heat, fade resistant resin fabrication process
- Extreme lightweight to strength ratio
- Made in the USA
- Badass looks for your BRZ or FR-S engine bay!
Lancia Hyena:
Overview:
ManufacturerZagato on Lancia mechanicals
Also calledLancia Delta Zagato Hyena
Production1992–1996
24 made
AssemblyRho, Milan
DesignerMarco Pedracini at Zagato
Body and chassis
ClassSports car
Body style2-door coupé
LayoutTransverse front-engine, four-wheel drive
RelatedLancia Delta Integrale "Evoluzione"
Powertrain
Engine2.0 L I4 (turbocharged petrol)
Transmission5-speed manual
The Lancia Hyena was a 2-door coupé made in small numbers by Italian coachbuilder Zagato on the basis of the Delta HF Integrale "Evoluzione".
History:
The Hyena was born thanks to the initiative of Dutch classic car restorer and collector Paul V.J. Koot, who desired a coupé version of the multiple World Rally Champion HF Integrale. He turned to Zagato, where Hyena was designed in 1990 by Marco Pedracini. A first prototype was introduced at the Brussels Motor Show in January 1992.
Decision was taken to put the Hyena into limited production. Fiat refused to participate in the project supplying bare HF Integrale chassis, which complicated the manufacturing process: the Hyena had to be produced from fully finished HF Integrales, privately purchased at Lancia dealers. Koot's Lusso Service took care of procuring and stripping the donor cars in the Netherlands; they were then sent to Zagato in Milan to have the new body built and for final assembly. All of this made the Hyena very expensive to build and they were sold for around 140,000 Swiss francs or $75,000 (£49,430).
A production run of 75 examples was initially planned, but only 25 Hyenas were completed between 1992 and 1993.
Specifications:
The Zagato bodywork made use of aluminium alloys and composite materials; the interior featured new dashboard, console and door cards made entirely from carbon fibre. Thanks to these weight saving measures the Hyena was some 150 kilograms (330 lb) lighter than the original HF Integrale, about 15% of its overall weight. The two-litre turbo engine was upgraded from 205 to 250 PS (184 kW), and the car could accelerate from 0–100 km in 5.4 seconds.
[Text from Wikipedia]
en.wikipedia.org/wiki/Lancia_Delta#Lancia_Hyena
This miniland-scale Lego Lancia Hyena (1992 - Zagato) has been created for Flickr LUGNuts' 92nd Build Challenge, - "Stuck in the 90's", - all about vehicles from the decade of the 1990s.
Jelly Belly Candy Company, formerly known as Herman Goelitz Candy Company and Goelitz Confectionery Company, manufactures Jelly Belly jelly beans and other candy. It is based in Fairfield, California, with a second manufacturing facility in North Chicago, Illinois and a distribution center in Pleasant Prairie, Wisconsin. In October 2008, the company opened a 50,000 sq ft (4,645 m2) manufacturing plant in Rayong, Thailand where it produces confectionery for the international market.
The company's signature product, the Jelly Belly jelly bean, comes in more than 50 varieties, ranging from traditional flavors like orange, lemon, lime, and cherry, to more exotic ones like cinnamon, pomegranate, cappuccino, buttered popcorn, and chili-mango.
Jelly Belly Candy Company manufactures numerous specialty Jelly Belly jelly beans with licensed products like Tabasco sauce and uncommon candy tastes like egg nog and pancakes with maple syrup. A few flavors, like lychee and green tea, are sold only in markets outside the United States.
Several flavors have been based on popular alcoholic beverages, beginning with Mai Tai in 1977. Over the years, new additions have included blackberry brandy (now discontinued), strawberry daiquiri, margarita, mojito, and piña colada. Draft beer, a flavor inspired by Hefeweizen ale, was introduced in 2014. All such flavors are entirely alcohol-free.
"Bertie Bott's Every Flavour Beans" were inspired by the Harry Potter book series and featured intentionally gruesome flavors such as "Vomit", "Earwax", "Skunk Spray", and "Rotten Egg". A similar product pairs lookalike "normal" jelly beans with weird flavors in a product dubbed "BeanBoozled" which has gone through several editions.
"Sport Beans" are jelly beans designed to provide physical energy and enhance athletic performance. They contain carbohydrates, electrolytes (in the form of sodium and potassium), and vitamins B1, B2, B3 and C. "Extreme Sport Beans" include the additional boost of caffeine.
The company makes over 100 different confections, including chocolates, licorice, gummis, and candy corn.
The company operates three manufacturing plants in Fairfield, California; North Chicago, Illinois; and Rayong, Thailand. A fourth facility in Pleasant Prairie, Wisconsin, is for distribution.
The Fairfield and Pleasant Prairie locations offer free daily tours. The 1⁄4 mi-long (400 m) self-guided Fairfield tour features interactive exhibits, Jelly Belly bean art, and videos featuring the candy manufacturing process. It was named one of the best factory tours for children by FamilyFun Magazine in 2014.
en.wikipedia.org/wiki/Jelly_Belly
en.wikipedia.org/wiki/Wikipedia:Text_of_Creative_Commons_...
As part of the required course knowledge pupils need to be able to outline the process involved in taking a square wooden blank and preparing it for turning between centres. These pictures depict that process chronologically.
Stage 1 * Preparation of wooden blank. Cut to size. Sand square. Mark across diagonals. Centre punch the centre point. Use spring dividers to mark circumference. Repeat on other end.
Stage 2 * Plane off corners down to circumference line. This takes cross section from square to octagon. This reduces force on cutting toll in initial prep of blank. Mount between fork [driven] centre and dead [or live ] centre at tailstock end. Apply grease a dead centre end. apply force from tailstock end to force fork into material at driven end. Adjust toolstock height to suit. Check for clearance.
Stage 3 * Roughout using scraper to diameter. Use combination of gouges and skew chisels to add beads and other decorative detailing as required. Ensure spindle speed is appropriate for material and cross section under consideration. Obey all safety instructions.
Jelly Belly Candy Company, formerly known as Herman Goelitz Candy Company and Goelitz Confectionery Company, manufactures Jelly Belly jelly beans and other candy. It is based in Fairfield, California, with a second manufacturing facility in North Chicago, Illinois and a distribution center in Pleasant Prairie, Wisconsin. In October 2008, the company opened a 50,000 sq ft (4,645 m2) manufacturing plant in Rayong, Thailand where it produces confectionery for the international market.
The company's signature product, the Jelly Belly jelly bean, comes in more than 50 varieties, ranging from traditional flavors like orange, lemon, lime, and cherry, to more exotic ones like cinnamon, pomegranate, cappuccino, buttered popcorn, and chili-mango.
Jelly Belly Candy Company manufactures numerous specialty Jelly Belly jelly beans with licensed products like Tabasco sauce and uncommon candy tastes like egg nog and pancakes with maple syrup. A few flavors, like lychee and green tea, are sold only in markets outside the United States.
Several flavors have been based on popular alcoholic beverages, beginning with Mai Tai in 1977. Over the years, new additions have included blackberry brandy (now discontinued), strawberry daiquiri, margarita, mojito, and piña colada. Draft beer, a flavor inspired by Hefeweizen ale, was introduced in 2014. All such flavors are entirely alcohol-free.
"Bertie Bott's Every Flavour Beans" were inspired by the Harry Potter book series and featured intentionally gruesome flavors such as "Vomit", "Earwax", "Skunk Spray", and "Rotten Egg". A similar product pairs lookalike "normal" jelly beans with weird flavors in a product dubbed "BeanBoozled" which has gone through several editions.
"Sport Beans" are jelly beans designed to provide physical energy and enhance athletic performance. They contain carbohydrates, electrolytes (in the form of sodium and potassium), and vitamins B1, B2, B3 and C. "Extreme Sport Beans" include the additional boost of caffeine.
The company makes over 100 different confections, including chocolates, licorice, gummis, and candy corn.
The company operates three manufacturing plants in Fairfield, California; North Chicago, Illinois; and Rayong, Thailand. A fourth facility in Pleasant Prairie, Wisconsin, is for distribution.
The Fairfield and Pleasant Prairie locations offer free daily tours. The 1⁄4 mi-long (400 m) self-guided Fairfield tour features interactive exhibits, Jelly Belly bean art, and videos featuring the candy manufacturing process. It was named one of the best factory tours for children by FamilyFun Magazine in 2014.
en.wikipedia.org/wiki/Jelly_Belly
en.wikipedia.org/wiki/Wikipedia:Text_of_Creative_Commons_...
Io Aircraft - www.ioaircraft.com
Drew Blair
www.linkedin.com/in/drew-b-25485312/
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
ABERDEEN PROVING GROUND, Md. (Dec. 19, 2014) -- The U.S. Army is seeking to implement a new mortar manufacturing process to provide improved weapons at a lower cost, officials said.
The Army introduced a nickel super-alloy called Inconcel to produce mortars in 2008, but its properties make it challenging to manufacture. Researchers have been working on an alternative method to overcome the difficulties, said Chris Humiston, a mechanical engineer with the Armament Research, Development and Engineering Center at Watervliet Arsenal, New York.
Read more:
This image shows the Parkside works of the Edinburgh publishing firm Thomas Nelsons. Until its closure in 1968 Thomas Nelsons was one of the most successful publishing houses in the world. The company had been trading in Edinburgh since 1798 when Thomas Nelson established a second-hand bookshop at the West Bow. The experience as a bookseller convinced Thomas of the existence of a ready market for cheap, standard editions of non-copyright works, and he satisfied it by issuing popular editions of classics.However, with the building in 1845 of a new printing house at Hope Park, the complete book manufacturing process was carried out under one roof, with a pay-roll of over four hundred employees.
A fire devastated Hope Park in 1878, causing damage estimated between £100,000 and £200,000. Within two months Thomas Nelson and Sons were back in operation, albeit on a limited scale. Within two years the production works moved to a new site at Parkside near the brothers’ own properties. The calamity at Hope Park had brought the fortuitous benefit of investment in new plant from which a flood of reprints, schoolbooks, prize books and religious books poured – all at inexpensive prices. The New Factory, capable of producing 200,000 books a week, was built at Parkside in 1907 to undertake the various Classics series. It stood in extensive grounds facing the Dalkeith Road, Edinburgh. The works themselves covered about five acres of ground and the New Factory an additional acre.
Parkside was equipped with the most modern printing and bindery machinery of their day as it was the aim that every process of book production should be undertaken within the factory. Many of the machines, especially in the bindery were constructed by the Nelsons. With the new space provided at Parkside, Thomas Nelson junior was able to investigate new processes including developing a surface paper. This paper was partly made by hand, for use with half tone blacks, a technique which was nearly as innovative as his development of the rotary press
Edinburgh City of Print is a joint project between the City of Edinburgh Museums and the Scottish Archive of Print and Publishing History Records (SAPPHIRE). The project aims to catalogue and make accessible the wealth of printing collections held by the City of Edinburgh Museums. For more information about the project please visit www.edinburghcityofprint.org
Image courtesy of SAPPHIRE
BlueEdge - Mach 8-10 Hypersonic Commercial Aircraft, 220 Passenger Hypersonic Commercial Plane - Iteration 3
Seating: 220 | Crew 2+4
Length: 195ft | Span: 93ft
Engines: 4 U-TBCC (Unified Turbine Based Combined Cycle) +1 Aerospike for sustained 2G acceleration to Mach 10.
Fuel: H2 (Compressed Hydrogen)
Cruising Altitude: 100,000-125,000ft
Airframe: 75% Proprietary Composites
Operating Costs, Similar to a 737. $7,000-$15,000hr, including averaged maintenence costs
Iteration 3 (Full release of IT3, Monday January 14, 2019)
IO Aircraft www.ioaircraft.com
Drew Blair www.linkedin.com/in/drew-b-25485312/
-----------------------------
hypersonic plane, hypersonic aircraft, hypersonic commercial plane, hypersonic commercial aircraft, hypersonic airline, tbcc, glide breaker, fighter plane, hyperonic fighter, boeing phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, office of naval research, defense advanced research project agency, defense science, missile defense agency, aerospike, hydrogen, hydrogen storage, hydrogen fueled, hydrogen aircraft, virgin airlines, united airlines, sas, finnair ,emirates airlines, ANA, JAL, airlines, military, physics, airline, british airways, air france
-----------------------------
Unified Turbine Based Combined Cycle. Current technologies and what Lockheed is trying to force on the Dept of Defense, for that low speed Mach 5 plane DOD gave them $1 billion to build and would disintegrate above Mach 5, is TBCC. 2 separate propulsion systems in the same airframe, which requires TWICE the airframe space to use.
Unified Turbine Based Combined Cycle is 1 propulsion system cutting that airframe deficit in half, and also able to operate above Mach 10 up to Mach 15 in atmosphere, and a simple nozzle modification allows for outside atmosphere rocket mode, ie orbital capable.
Additionally, Reaction Engines maximum air breather mode is Mach 4.5, above that it will explode in flight from internal pressures are too high to operate. Thus, must switch to non air breather rocket mode to operate in atmosphere in hypersonic velocities. Which as a result, makes it not feasible for anything practical. It also takes an immense amount of fuel to function.
-------------
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
8th Gen Mach 8-10 Hypersonic Fighter Plane - Silver Hawk - IO Aircraft
I doubt I will post this again or details of this, since details are immense and shouldn't enter the public realm. Needless to say, Mach 8-10 8th Gen Super Fighter, details omitted, uses about the same aero/thermo-dynamics as Ranger. But its a lot bigger, not VTOL, and meant for manned or unmanned. It is not a graphics illustration. ANYS, Openfoam, Combined Cycle propulsion systems, etc etc. heavily sanitized so it cant be reverse engineered. --> www.ioaircraft.com/
www.ioaircraft.com/hypersonic/ranger.php
Drew Blair
www.linkedin.com/in/drew-b-25485312/
-------------
glide breaker, fighter plane, hyperonic fighter, stealth fighter, boeing phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, office of naval research, defense advanced research project agency, defense science, missile defense agency, aerospike, vtol, vertical take off, air taxi, personal air vehicle, boeing go fly prize, go fly prize,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
I love the shape of these 1960s glass. So modern in their clean design lines, yet the amber glass is totally retro. What is impossible to see in the photographs is the small air bubbles and actuals lines in the glass from the manufacturing process. They are beautiful just to hold up to the light and examine. If you didn't want to use them as glasses they would look beautiful on a window ledge as bud vases.
Each glass stands 5 inches tall by 2 inches wide.
Lancia Hyena:
Overview:
ManufacturerZagato on Lancia mechanicals
Also calledLancia Delta Zagato Hyena
Production1992–1996
24 made
AssemblyRho, Milan
DesignerMarco Pedracini at Zagato
Body and chassis
ClassSports car
Body style2-door coupé
LayoutTransverse front-engine, four-wheel drive
RelatedLancia Delta Integrale "Evoluzione"
Powertrain
Engine2.0 L I4 (turbocharged petrol)
Transmission5-speed manual
The Lancia Hyena was a 2-door coupé made in small numbers by Italian coachbuilder Zagato on the basis of the Delta HF Integrale "Evoluzione".
History:
The Hyena was born thanks to the initiative of Dutch classic car restorer and collector Paul V.J. Koot, who desired a coupé version of the multiple World Rally Champion HF Integrale. He turned to Zagato, where Hyena was designed in 1990 by Marco Pedracini. A first prototype was introduced at the Brussels Motor Show in January 1992.
Decision was taken to put the Hyena into limited production. Fiat refused to participate in the project supplying bare HF Integrale chassis, which complicated the manufacturing process: the Hyena had to be produced from fully finished HF Integrales, privately purchased at Lancia dealers. Koot's Lusso Service took care of procuring and stripping the donor cars in the Netherlands; they were then sent to Zagato in Milan to have the new body built and for final assembly. All of this made the Hyena very expensive to build and they were sold for around 140,000 Swiss francs or $75,000 (£49,430).
A production run of 75 examples was initially planned, but only 25 Hyenas were completed between 1992 and 1993.
Specifications:
The Zagato bodywork made use of aluminium alloys and composite materials; the interior featured new dashboard, console and door cards made entirely from carbon fibre. Thanks to these weight saving measures the Hyena was some 150 kilograms (330 lb) lighter than the original HF Integrale, about 15% of its overall weight. The two-litre turbo engine was upgraded from 205 to 250 PS (184 kW), and the car could accelerate from 0–100 km in 5.4 seconds.
[Text from Wikipedia]
en.wikipedia.org/wiki/Lancia_Delta#Lancia_Hyena
This miniland-scale Lego Lancia Hyena (1992 - Zagato) has been created for Flickr LUGNuts' 92nd Build Challenge, - "Stuck in the 90's", - all about vehicles from the decade of the 1990s.
Jelly Belly Candy Company, formerly known as Herman Goelitz Candy Company and Goelitz Confectionery Company, manufactures Jelly Belly jelly beans and other candy. It is based in Fairfield, California, with a second manufacturing facility in North Chicago, Illinois and a distribution center in Pleasant Prairie, Wisconsin. In October 2008, the company opened a 50,000 sq ft (4,645 m2) manufacturing plant in Rayong, Thailand where it produces confectionery for the international market.
The company's signature product, the Jelly Belly jelly bean, comes in more than 50 varieties, ranging from traditional flavors like orange, lemon, lime, and cherry, to more exotic ones like cinnamon, pomegranate, cappuccino, buttered popcorn, and chili-mango.
Jelly Belly Candy Company manufactures numerous specialty Jelly Belly jelly beans with licensed products like Tabasco sauce and uncommon candy tastes like egg nog and pancakes with maple syrup. A few flavors, like lychee and green tea, are sold only in markets outside the United States.
Several flavors have been based on popular alcoholic beverages, beginning with Mai Tai in 1977. Over the years, new additions have included blackberry brandy (now discontinued), strawberry daiquiri, margarita, mojito, and piña colada. Draft beer, a flavor inspired by Hefeweizen ale, was introduced in 2014. All such flavors are entirely alcohol-free.
"Bertie Bott's Every Flavour Beans" were inspired by the Harry Potter book series and featured intentionally gruesome flavors such as "Vomit", "Earwax", "Skunk Spray", and "Rotten Egg". A similar product pairs lookalike "normal" jelly beans with weird flavors in a product dubbed "BeanBoozled" which has gone through several editions.
"Sport Beans" are jelly beans designed to provide physical energy and enhance athletic performance. They contain carbohydrates, electrolytes (in the form of sodium and potassium), and vitamins B1, B2, B3 and C. "Extreme Sport Beans" include the additional boost of caffeine.
The company makes over 100 different confections, including chocolates, licorice, gummis, and candy corn.
The company operates three manufacturing plants in Fairfield, California; North Chicago, Illinois; and Rayong, Thailand. A fourth facility in Pleasant Prairie, Wisconsin, is for distribution.
The Fairfield and Pleasant Prairie locations offer free daily tours. The 1⁄4 mi-long (400 m) self-guided Fairfield tour features interactive exhibits, Jelly Belly bean art, and videos featuring the candy manufacturing process. It was named one of the best factory tours for children by FamilyFun Magazine in 2014.
en.wikipedia.org/wiki/Jelly_Belly
en.wikipedia.org/wiki/Wikipedia:Text_of_Creative_Commons_...
What an amazing company Morgan are. Ever since they cocked a snook at Sir John Harvey-Jones' view of their manufacturing processes, they have gone from strength to strength and these days build a unique and highly desirable array of both modern and classic-style models. With the LIFECar, they have a toe firmly in the future too and, having recently celebrated their first centenary, seem all set to enjoy a second one. The list of marques that have come and gone since they were born is long indeed. Moreover, the company is still managed by a member of the Morgan family - Charles Morgan, the grandson of the founder, Henry Frederick Stanley Morgan.
Never scared of being controversial, Morgan certainly caused a stir when they launched the cross-eyed Aero 8 in 2001 - their first new model since 1948. Some loved the looks and some didn't, but what was beyond debate was that the car bristled with technology and performance to a level few could have expected from a small volume manufacturer best known for designs whose roots lay in the 1930s. Gone was the traditional Morgan steel chassis topped by an alloy-skinned wooden body tub. Instead, the car boasted an ultra-modern alloy chassis, while power came courtesy of a thumping BMW V8 - initially of 4.4-litres and now of 4.8-litres.
By 2004, the company's desire to succeed in the USA was necessitating cars with a softer edge and more creature comforts. What better time to appease those in search of ever more raw power than by building a limited run of real fire-breathing monsters inspired by their participation at Le Mans - enter the Aero 8 GTN.
In fact just 11 GTNs were made for sale. A lightweight body ensured an all-up weight of just one ton, while power came courtesy of a 4.6-litre BMW V8 engine producing 330bhp. 330bhp/ton is enough to make a car go very quickly and the GTN did, reaching 60mph in around 4.3 seconds and progressing to a top speed of around 170mph. The sound emitted in the process was music indeed.
VX53 KTJ was No.4 of the 11 GTNs made and the very car tested by Richard Hammond (himself the proud owner of an Aeromax, the Coupe version of the Aero 8) and The Stig for BBC2's Top Gear (see You Tube clip www.youtube.com/watch?v=ACEo-CwV63w) and covered for the Sunday Times by Rob Brydon in place of a holidaying Jeremy Clarkson. With bodywork in blue over silver and a black leather interior, it looks suitably lean and mean. Extras on this amazing car include: radio/CD, side exit sports exhausts, Moto-Lita steering wheel, carbonfibre fascia and hardtop, air conditioning and black Centre Lock OZ alloy wheels.
In the heart of Old Town, historic factory is among the oldest in Grasse ... Indeed the current premises sheltered from their beginning in 1782, a perfume factory. In 1926, after the famous painter Jean Honoré Fragonard, it takes the name of Parfumerie Fragonard. Since then, every day, we produce are our perfumes, cosmetics and soaps in a respectful environment of tradition. We would be happy to welcome you and offer you a guided tour during which you will discover the different manufacturing processes and packaging our products. At the end of your visit, you can admire 3000 years of history of perfume through our private museum.
Dedicated to the perfume and aromatic plants, Flower Factory is surrounded by a beautiful garden scented plants ... the gates of Grasse, this contemporary factory opened in 1986 is equipped with very modern machinery for the manufacture and packaging of our products.
WORKSHOP ODOR "Perfumer's Apprentice"
Available on the French Riviera and Paris, in factories, workshops Perfumers Apprentice can discover the expertise of Perfumer: the history of perfume, raw materials and different extraction methods.
Experience unforgettable sense centered on the composition of a toilet water (100 ml) in aromatic notes of citrus and orange blossom, by assembling the different species made available. A fun and exciting experience in the world of perfumery, which proposes the course led by the teacher, the bottle and its bag, apron "apprentice" printed Fragonard, the diploma signed by the teacher and the summary of the composition .
One of our guides will accompany you as a result of the workshop for a visit "Prestige" from our factory.
Located in one of the oldest houses in the historic center of the city, this perfume offers original creations of Didier Gaglewski.
Didier Gaglewski, "nose" in Grasse, began offering its achievements in the framework Living in Provence and in Paris, Germany and Switzerland. Both "artisan", "artist", he decided to offer his achievements directly driven by the idea that the quality, originality and respect perfume composition will dress with fun, humor and quality its customers.
Requiring each of its perfumes, made in the privacy of his laboratory, took several months of research. In partnership with Michelle Cavalier and the "garden of La Bastide," Didier Gaglewski also remains closer to the flowers and working the land. Try to trace extraction techniques inherited from the past and plants specific to the region perfumes seduce and make a very personal and authentic. This atypical creator is distinguished by its compositions made in Grasse basin, its choice to favor natural raw materials and the search for sobriety.
Front satisfaction and customer demands wishing to regain the proposed perfumes, shop in Grasse, 12 rue of the Oratory, just steps from the International Perfume Museum to discover the scents and recent creations.
The country house of Aromas
Based in Saint Cézaire on Siagne in the Pays de Grasse, the Bastide aromas manufactures and packages fragrances since 1995.
Saint Cézaire on Siagne is a typical Provencal village a few kilometers from Grasse, the world capital of perfumery.
The homemade studio human scale can meet all your demands. The 100% handmade is carried out in the workshop without intermediary, under the control of a chemist.
La Bastide des Aromas, respects the traditions of the Grasse region and offers the exclusive fragrances custom made in the workshop on-site, high quality, with particular stress on the fragrance concentration, her outfit and originality.
In the heart of Old Town, historic factory is among the oldest in Grasse ... Indeed the current premises sheltered from their beginning in 1782, a perfume factory. In 1926, after the famous painter Jean Honoré Fragonard, it takes the name of Parfumerie Fragonard. Since then, every day, we produce are our perfumes, cosmetics and soaps in a respectful environment of tradition. We would be happy to welcome you and offer you a guided tour during which you will discover the different manufacturing processes and packaging our products. At the end of your visit, you can admire 3000 years of history of perfume through our private museum.
Dedicated to the perfume and aromatic plants, Flower Factory is surrounded by a beautiful garden scented plants ... the gates of Grasse, this contemporary factory opened in 1986 is equipped with very modern machinery for the manufacture and packaging of our products.
WORKSHOP ODOR "Perfumer's Apprentice"
Available on the French Riviera and Paris, in factories, workshops Perfumers Apprentice can discover the expertise of Perfumer: the history of perfume, raw materials and different extraction methods.
Experience unforgettable sense centered on the composition of a toilet water (100 ml) in aromatic notes of citrus and orange blossom, by assembling the different species made available. A fun and exciting experience in the world of perfumery, which proposes the course led by the teacher, the bottle and its bag, apron "apprentice" printed Fragonard, the diploma signed by the teacher and the summary of the composition .
One of our guides will accompany you as a result of the workshop for a visit "Prestige" from our factory.
Located in one of the oldest houses in the historic center of the city, this perfume offers original creations of Didier Gaglewski.
Didier Gaglewski, "nose" in Grasse, began offering its achievements in the framework Living in Provence and in Paris, Germany and Switzerland. Both "artisan", "artist", he decided to offer his achievements directly driven by the idea that the quality, originality and respect perfume composition will dress with fun, humor and quality its customers.
Requiring each of its perfumes, made in the privacy of his laboratory, took several months of research. In partnership with Michelle Cavalier and the "garden of La Bastide," Didier Gaglewski also remains closer to the flowers and working the land. Try to trace extraction techniques inherited from the past and plants specific to the region perfumes seduce and make a very personal and authentic. This atypical creator is distinguished by its compositions made in Grasse basin, its choice to favor natural raw materials and the search for sobriety.
Front satisfaction and customer demands wishing to regain the proposed perfumes, shop in Grasse, 12 rue of the Oratory, just steps from the International Perfume Museum to discover the scents and recent creations.
The country house of Aromas
Based in Saint Cézaire on Siagne in the Pays de Grasse, the Bastide aromas manufactures and packages fragrances since 1995.
Saint Cézaire on Siagne is a typical Provencal village a few kilometers from Grasse, the world capital of perfumery.
The homemade studio human scale can meet all your demands. The 100% handmade is carried out in the workshop without intermediary, under the control of a chemist.
La Bastide des Aromas, respects the traditions of the Grasse region and offers the exclusive fragrances custom made in the workshop on-site, high quality, with particular stress on the fragrance concentration, her outfit and originality.
The United States Astronaut Hall of Fame, located inside the Kennedy Space Center Visitor Complex Heroes & Legends building on Merritt Island, Florida, honors American astronauts and features the world's largest collection of their personal memorabilia, focusing on those astronauts who have been inducted into the Hall. Exhibits include Wally Schirra's Sigma 7 space capsule from the fifth crewed Mercury mission and the Gemini IX spacecraft flown by Gene Cernan and Thomas P. Stafford in 1966.
In the 1980s, the six then-surviving Mercury Seven astronauts conceived of establishing a place where US space travelers could be remembered and honored, along the lines of halls of fame for other fields. The Mercury Seven Foundation and Astronaut Scholarship Foundation were formed, and have a role in the ongoing operations of the Hall of Fame. The foundation's first executive director was former Associated Press space reporter Howard Benedict.
The Astronaut Hall of Fame was opened on October 29, 1990, by the U.S. Space Camp Foundation, which was the first owner of the facility. It was located next to the Florida branch of Space Camp.
The Hall of Fame closed for several months in 2002 when U.S. Space Camp Foundation's creditors foreclosed on the property due to low attendance and mounting debt. That September, an auction was held and the property was purchased by Delaware North Park Services on behalf of NASA and the property was added to the Kennedy Space Center Visitor Complex. The Hall of Fame re-opened December 14, 2002.
The Hall of Fame, which was originally located just west of the NASA Causeway, closed to the public on November 2, 2015, in preparation for its relocation to the Kennedy Space Center Visitor Complex 6 miles (9.7 km) to the east on Merritt Island. Outside of the original building was a full-scale replica of a Space Shuttle orbiter named Inspiration (originally named "Shuttle To Tomorrow" where visitors could enter and view a program). Inspiration served only as an outdoor, full scale, static display which visitors could not enter. After the Hall of Fame was transferred to the KSC Visitor Complex, Inspiration was acquired by LVX System and was placed in storage at the Shuttle Landing Facility at the Kennedy Space Center; in 2016, the shuttle was loaded on to a barge to be taken for refurbishment before going on an educational tour.
The building was purchased at auction by visitor complex operator Delaware North and renamed the ATX Center, and for a time housed educational programs including Camp Kennedy Space Center and the Astronaut Training Experience. Those programs have since been moved to the KSC Visitor Complex, and as of December 2019, the structure was being offered for lease. In July 2020, Lockheed Martin announced it would lease the building to support work on the NASA Orion crew capsule.
Inductees into the Hall of Fame are selected by a blue ribbon committee of former NASA officials and flight controllers, historians, journalists, and other space authorities (including former astronauts) based on their accomplishments in space or their contributions to the advancement of space exploration. Except for 2002, inductions have been held every year since 2001.
As its inaugural class in 1990, the Hall of Fame inducted the United States' original group of astronauts: the Mercury Seven. In addition to being the first American astronauts, they set several firsts in American spaceflight, both auspicious and tragic. Alan Shepard was the first American in space and later became one of the twelve people to walk on the Moon. John Glenn was the first American to orbit the Earth and after his induction went on, in 1998, to become the oldest man to fly in space, aged 77. Gus Grissom was the first American to fly in space twice and was the commander of the ill-fated Apollo 1, which resulted in the first astronaut deaths directly related to preparation for spaceflight.
Thirteen astronauts from the Gemini and Apollo programs were inducted in the second class of 1993. This class included the first and last humans to walk on the Moon, Neil Armstrong and Eugene Cernan; Ed White, the first American to walk in space (also killed in the Apollo 1 accident); Jim Lovell, commander of the famously near-tragic Apollo 13; and John Young, whose six flights included a moonwalk and command of the first Space Shuttle mission.
The third class was inducted in 1997 and consisted of the 24 additional Apollo, Skylab, and ASTP astronauts. Notable members of the class were Roger Chaffee, the third astronaut killed in the Apollo 1 fire and the only unflown astronaut in the Hall; Harrison Schmitt, the first scientist and next-to-last person to walk on the Moon; and Jack Swigert and Fred Haise, the Apollo 13 crewmembers not previously inducted.
The philosophy regarding the first three groups of inductees was that all astronauts who flew in NASA's "pioneering" programs (which would include Mercury, Gemini, Apollo, Apollo Applications Program (Skylab), and Apollo-Soyuz Test Project) would be included simply by virtue of their participation in a spaceflight in these early programs. The first group (the inaugural class of 1990) would only include the original Mercury astronauts (most of whom would go on to fly in later programs). The second group of inductees would include those astronauts who began their spaceflight careers during Gemini (all of whom would go on to fly in later programs). The third group of inductees would include those astronauts who began their spaceflight careers during Apollo, Skylab, and ASTP (some of whom would go on to fly in the Space Shuttle program). Since it would not be practical (or meaningful) to induct all astronauts who ever flew in space, all subsequent inductees (Space Shuttle program and beyond) are considered based on their accomplishments and contributions to the human spaceflight endeavor which would set them apart from their peers.
Over four dozen astronauts from the Space Shuttle program have been inducted since 2001. Among these are Sally Ride, the first American woman in space; Story Musgrave, who flew six missions in the 1980s and 90s; and Francis Scobee, commander of the ill-fated final Challenger mission.
The 2010 class consisted of Guion Bluford Jr., Kenneth Bowersox, Frank Culbertson and Kathryn Thornton. The 2011 inductees were Karol Bobko and Susan Helms. The 2012 inductees were Franklin Chang-Diaz, Kevin Chilton and Charles Precourt. Bonnie Dunbar, Curt Brown and Eileen Collins were inducted in 2013, and Shannon Lucid and Jerry Ross comprised the 2014 class.
Those inducted in 2015 were John Grunsfeld, Steven Lindsey, Kent Rominger, and Rhea Seddon. In 2016, inductees included Brian Duffy and Scott E. Parazynski. Ellen Ochoa and Michael Foale were announced as the 2017 class of the United States Astronaut Hall of Fame. Scott Altman and Thomas Jones followed in 2018. The 2019 inductees were James Buchli and Janet L. Kavandi.
Michael López-Alegría, Scott Kelly and Pamela Melroy were the 2020 inductees, inducted in a November 2021 ceremony. The 2022 inductees were Christopher Ferguson, David Leestma, and Sandra Magnus. Roy Bridges Jr. and Mark Kelly were the 2023 inductees.
The Hall of Heroes is composed of tributes to the inductees. Among the Hall of Fame's displays is Sigma 7, the Mercury spacecraft piloted by Wally Schirra which orbited the Earth six times in 1962, and the Gemini 9A capsule flown by Gene Cernan and Thomas P. Stafford in 1966. An Astronaut Adventure room includes simulators for use by children.
The spacesuit worn by Gus Grissom during his 1961 Liberty Bell 7 Mercury flight is on display and has been the subject of a dispute between NASA and Grissom's heirs and supporters since 2002. The spacesuit, along with other Grissom artifacts, were loaned to the original owners of the Hall of Fame by the Grissom family when it opened. After the Hall of Fame went into bankruptcy and was taken over by a NASA contractor in 2002, the family requested that all their items be returned. All of the items were returned to Grissom's family except the spacesuit, because both NASA and the Grissoms claim ownership of it. NASA claims Grissom checked out the spacesuit for a show and tell at his son's school, and then never returned it, while the Grissoms claim Gus rescued the spacesuit from a scrap heap.
The John F. Kennedy Space Center (KSC, originally known as the NASA Launch Operations Center), located on Merritt Island, Florida, is one of the National Aeronautics and Space Administration's (NASA) ten field centers. Since December 1968, KSC has been NASA's primary launch center of human spaceflight. Launch operations for the Apollo, Skylab and Space Shuttle programs were carried out from Kennedy Space Center Launch Complex 39 and managed by KSC.[4] Located on the east coast of Florida, KSC is adjacent to Cape Canaveral Space Force Station (CCSFS). The management of the two entities work very closely together, share resources and operate facilities on each other's property.
Though the first Apollo flights and all Project Mercury and Project Gemini flights took off from the then-Cape Canaveral Air Force Station, the launches were managed by KSC and its previous organization, the Launch Operations Directorate. Starting with the fourth Gemini mission, the NASA launch control center in Florida (Mercury Control Center, later the Launch Control Center) began handing off control of the vehicle to the Mission Control Center in Houston, shortly after liftoff; in prior missions it held control throughout the entire mission.
Additionally, the center manages launch of robotic and commercial crew missions and researches food production and In-Situ Resource Utilization for off-Earth exploration. Since 2010, the center has worked to become a multi-user spaceport through industry partnerships, even adding a new launch pad (LC-39C) in 2015.
There are about 700 facilities and buildings grouped across the center's 144,000 acres (580 km2). Among the unique facilities at KSC are the 525-foot (160 m) tall Vehicle Assembly Building for stacking NASA's largest rockets, the Launch Control Center, which conducts space launches at KSC, the Operations and Checkout Building, which houses the astronauts dormitories and suit-up area, a Space Station factory, and a 3-mile (4.8 km) long Shuttle Landing Facility. There is also a Visitor Complex open to the public on site.
Since 1949, the military had been performing launch operations at what would become Cape Canaveral Space Force Station. In December 1959, the Department of Defense transferred 5,000 personnel and the Missile Firing Laboratory to NASA to become the Launch Operations Directorate under NASA's Marshall Space Flight Center.
President John F. Kennedy's 1961 goal of a crewed lunar landing by 1970 required an expansion of launch operations. On July 1, 1962, the Launch Operations Directorate was separated from MSFC to become the Launch Operations Center (LOC). Also, Cape Canaveral was inadequate to host the new launch facility design required for the mammoth 363-foot (111 m) tall, 7,500,000-pound-force (33,000 kN) thrust Saturn V rocket, which would be assembled vertically in a large hangar and transported on a mobile platform to one of several launch pads. Therefore, the decision was made to build a new LOC site located adjacent to Cape Canaveral on Merritt Island.
NASA began land acquisition in 1962, buying title to 131 square miles (340 km2) and negotiating with the state of Florida for an additional 87 square miles (230 km2). The major buildings in KSC's Industrial Area were designed by architect Charles Luckman. Construction began in November 1962, and Kennedy visited the site twice in 1962, and again just a week before his assassination on November 22, 1963.
On November 29, 1963, the facility was given its current name by President Lyndon B. Johnson under Executive Order 11129. Johnson's order joined both the civilian LOC and the military Cape Canaveral station ("the facilities of Station No. 1 of the Atlantic Missile Range") under the designation "John F. Kennedy Space Center", spawning some confusion joining the two in the public mind. NASA Administrator James E. Webb clarified this by issuing a directive stating the Kennedy Space Center name applied only to the LOC, while the Air Force issued a general order renaming the military launch site Cape Kennedy Air Force Station.
Located on Merritt Island, Florida, the center is north-northwest of Cape Canaveral on the Atlantic Ocean, midway between Miami and Jacksonville on Florida's Space Coast, due east of Orlando. It is 34 miles (55 km) long and roughly six miles (9.7 km) wide, covering 219 square miles (570 km2). KSC is a major central Florida tourist destination and is approximately one hour's drive from the Orlando area. The Kennedy Space Center Visitor Complex offers public tours of the center and Cape Canaveral Space Force Station.
The KSC Industrial Area, where many of the center's support facilities are located, is 5 miles (8 km) south of LC-39. It includes the Headquarters Building, the Operations and Checkout Building and the Central Instrumentation Facility. The astronaut crew quarters are in the O&C; before it was completed, the astronaut crew quarters were located in Hangar S[39] at the Cape Canaveral Missile Test Annex (now Cape Canaveral Space Force Station). Located at KSC was the Merritt Island Spaceflight Tracking and Data Network station (MILA), a key radio communications and spacecraft tracking complex.
Facilities at the Kennedy Space Center are directly related to its mission to launch and recover missions. Facilities are available to prepare and maintain spacecraft and payloads for flight. The Headquarters (HQ) Building houses offices for the Center Director, library, film and photo archives, a print shop and security. When the KSC Library first opened, it was part of the Army Ballistic Missile Agency. However, in 1965, the library moved into three separate sections in the newly opened NASA headquarters before eventually becoming a single unit in 1970. The library contains over four million items related to the history and the work at Kennedy. As one of ten NASA center libraries in the country, their collection focuses on engineering, science, and technology. The archives contain planning documents, film reels, and original photographs covering the history of KSC. The library is not open to the public but is available for KSC, Space Force, and Navy employees who work on site. Many of the media items from the collection are digitized and available through NASA's KSC Media Gallery or through their more up-to-date Flickr gallery.
A new Headquarters Building was completed in 2019 as part of the Central Campus consolidation. Groundbreaking began in 2014.
The center operated its own 17-mile (27 km) short-line railroad. This operation was discontinued in 2015, with the sale of its final two locomotives. A third had already been donated to a museum. The line was costing $1.3 million annually to maintain.
The Kennedy Space Center Visitor Complex, operated by Delaware North since 1995, has a variety of exhibits, artifacts, displays and attractions on the history and future of human and robotic spaceflight. Bus tours of KSC originate from here. The complex also includes the separate Apollo/Saturn V Center, north of the VAB and the United States Astronaut Hall of Fame, six miles west near Titusville. There were 1.5 million visitors in 2009. It had some 700 employees.
It was announced on May 29, 2015, that the Astronaut Hall of Fame exhibit would be moved from its current location to another location within the Visitor Complex to make room for an upcoming high-tech attraction entitled "Heroes and Legends". The attraction, designed by Orlando-based design firm Falcon's Treehouse, opened November 11, 2016.
In March 2016, the visitor center unveiled the new location of the iconic countdown clock at the complex's entrance; previously, the clock was located with a flagpole at the press site. The clock was originally built and installed in 1969 and listed with the flagpole in the National Register of Historic Places in January 2000. In 2019, NASA celebrated the 50th anniversary of the Apollo program, and the launch of Apollo 10 on May 18. In summer of 2019, Lunar Module 9 (LM-9) was relocated to the Apollo/Saturn V Center as part of an initiative to rededicate the center and celebrate the 50th anniversary of the Apollo Program.
The John F. Kennedy Space Center (KSC, originally known as the NASA Launch Operations Center), located on Merritt Island, Florida, is one of the National Aeronautics and Space Administration's (NASA) ten field centers. Since December 1968, KSC has been NASA's primary launch center of American spaceflight, research, and technology. Launch operations for the Apollo, Skylab and Space Shuttle programs were carried out from Kennedy Space Center Launch Complex 39 and managed by KSC. Located on the east coast of Florida, KSC is adjacent to Cape Canaveral Space Force Station (CCSFS). The management of the two entities work very closely together, share resources and operate facilities on each other's property.
Though the first Apollo flights and all Project Mercury and Project Gemini flights took off from the then-Cape Canaveral Air Force Station, the launches were managed by KSC and its previous organization, the Launch Operations Directorate. Starting with the fourth Gemini mission, the NASA launch control center in Florida (Mercury Control Center, later the Launch Control Center) began handing off control of the vehicle to the Mission Control Center in Houston, shortly after liftoff; in prior missions it held control throughout the entire mission.
Additionally, the center manages launch of robotic and commercial crew missions and researches food production and in-situ resource utilization for off-Earth exploration. Since 2010, the center has worked to become a multi-user spaceport through industry partnerships, even adding a new launch pad (LC-39C) in 2015.
There are about 700 facilities and buildings grouped throughout the center's 144,000 acres (580 km2). Among the unique facilities at KSC are the 525-foot (160 m) tall Vehicle Assembly Building for stacking NASA's largest rockets, the Launch Control Center, which conducts space launches at KSC, the Operations and Checkout Building, which houses the astronauts dormitories and suit-up area, a Space Station factory, and a 3-mile (4.8 km) long Shuttle Landing Facility. There is also a Visitor Complex on site that is open to the public.
Since 1949, the military had been performing launch operations at what would become Cape Canaveral Space Force Station. In December 1959, the Department of Defense transferred 5,000 personnel and the Missile Firing Laboratory to NASA to become the Launch Operations Directorate under NASA's Marshall Space Flight Center.
President John F. Kennedy's 1961 goal of a crewed lunar landing by 1970 required an expansion of launch operations. On July 1, 1962, the Launch Operations Directorate was separated from MSFC to become the Launch Operations Center (LOC). Also, Cape Canaveral was inadequate to host the new launch facility design required for the mammoth 363-foot (111 m) tall, 7,500,000-pound-force (33,000 kN) thrust Saturn V rocket, which would be assembled vertically in a large hangar and transported on a mobile platform to one of several launch pads. Therefore, the decision was made to build a new LOC site located adjacent to Cape Canaveral on Merritt Island.
NASA began land acquisition in 1962, buying title to 131 square miles (340 km2) and negotiating with the state of Florida for an additional 87 square miles (230 km2). The major buildings in KSC's Industrial Area were designed by architect Charles Luckman. Construction began in November 1962, and Kennedy visited the site twice in 1962, and again just a week before his assassination on November 22, 1963.
On November 29, 1963, the facility was named by President Lyndon B. Johnson under Executive Order 11129. Johnson's order joined both the civilian LOC and the military Cape Canaveral station ("the facilities of Station No. 1 of the Atlantic Missile Range") under the designation "John F. Kennedy Space Center", spawning some confusion joining the two in the public mind. NASA Administrator James E. Webb clarified this by issuing a directive stating the Kennedy Space Center name applied only to the LOC, while the Air Force issued a general order renaming the military launch site Cape Kennedy Air Force Station.
Located on Merritt Island, Florida, the center is north-northwest of Cape Canaveral on the Atlantic Ocean, midway between Miami and Jacksonville on Florida's Space Coast, due east of Orlando. It is 34 miles (55 km) long and roughly six miles (9.7 km) wide, covering 219 square miles (570 km2). KSC is a major central Florida tourist destination and is approximately one hour's drive from the Orlando area. The Kennedy Space Center Visitor Complex offers public tours of the center and Cape Canaveral Space Force Station.
From 1967 through 1973, there were 13 Saturn V launches, including the ten remaining Apollo missions after Apollo 7. The first of two uncrewed flights, Apollo 4 (Apollo-Saturn 501) on November 9, 1967, was also the first rocket launch from KSC. The Saturn V's first crewed launch on December 21, 1968, was Apollo 8's lunar orbiting mission. The next two missions tested the Lunar Module: Apollo 9 (Earth orbit) and Apollo 10 (lunar orbit). Apollo 11, launched from Pad A on July 16, 1969, made the first Moon landing on July 20. The Apollo 11 launch included crewmembers Neil Armstrong, Michael Collins, and Buzz Aldrin, and attracted a record-breaking 650 million television viewers. Apollo 12 followed four months later. From 1970 to 1972, the Apollo program concluded at KSC with the launches of missions 13 through 17.
On May 14, 1973, the last Saturn V launch put the Skylab space station in orbit from Pad 39A. By this time, the Cape Kennedy pads 34 and 37 used for the Saturn IB were decommissioned, so Pad 39B was modified to accommodate the Saturn IB, and used to launch three crewed missions to Skylab that year, as well as the final Apollo spacecraft for the Apollo–Soyuz Test Project in 1975.
As the Space Shuttle was being designed, NASA received proposals for building alternative launch-and-landing sites at locations other than KSC, which demanded study. KSC had important advantages, including its existing facilities; location on the Intracoastal Waterway; and its southern latitude, which gives a velocity advantage to missions launched in easterly near-equatorial orbits. Disadvantages included: its inability to safely launch military missions into polar orbit, since spent boosters would be likely to fall on the Carolinas or Cuba; corrosion from the salt air; and frequent cloudy or stormy weather. Although building a new site at White Sands Missile Range in New Mexico was seriously considered, NASA announced its decision in April 1972 to use KSC for the shuttle. Since the Shuttle could not be landed automatically or by remote control, the launch of Columbia on April 12, 1981 for its first orbital mission STS-1, was NASA's first crewed launch of a vehicle that had not been tested in prior uncrewed launches.
In 1976, the VAB's south parking area was the site of Third Century America, a science and technology display commemorating the U.S. Bicentennial. Concurrent with this event, the U.S. flag was painted on the south side of the VAB. During the late 1970s, LC-39 was reconfigured to support the Space Shuttle. Two Orbiter Processing Facilities were built near the VAB as hangars with a third added in the 1980s.
KSC's 2.9-mile (4.7 km) Shuttle Landing Facility (SLF) was the orbiters' primary end-of-mission landing site, although the first KSC landing did not take place until the tenth flight, when Challenger completed STS-41-B on February 11, 1984; the primary landing site until then was Edwards Air Force Base in California, subsequently used as a backup landing site. The SLF also provided a return-to-launch-site (RTLS) abort option, which was not utilized. The SLF is among the longest runways in the world.
On October 28, 2009, the Ares I-X launch from Pad 39B was the first uncrewed launch from KSC since the Skylab workshop in 1973.
Beginning in 1958, NASA and military worked side by side on robotic mission launches (previously referred to as unmanned), cooperating as they broke ground in the field. In the early 1960s, NASA had as many as two robotic mission launches a month. The frequent number of flights allowed for quick evolution of the vehicles, as engineers gathered data, learned from anomalies and implemented upgrades. In 1963, with the intent of KSC ELV work focusing on the ground support equipment and facilities, a separate Atlas/Centaur organization was formed under NASA's Lewis Center (now Glenn Research Center (GRC)), taking that responsibility from the Launch Operations Center (aka KSC).
Though almost all robotics missions launched from the Cape Canaveral Space Force Station (CCSFS), KSC "oversaw the final assembly and testing of rockets as they arrived at the Cape." In 1965, KSC's Unmanned Launch Operations directorate became responsible for all NASA uncrewed launch operations, including those at Vandenberg Space Force Base. From the 1950s to 1978, KSC chose the rocket and payload processing facilities for all robotic missions launching in the U.S., overseeing their near launch processing and checkout. In addition to government missions, KSC performed this service for commercial and foreign missions also, though non-U.S. government entities provided reimbursement. NASA also funded Cape Canaveral Space Force Station launch pad maintenance and launch vehicle improvements.
All this changed with the Commercial Space Launch Act of 1984, after which NASA only coordinated its own and National Oceanic and Atmospheric Administration (NOAA) ELV launches. Companies were able to "operate their own launch vehicles" and utilize NASA's launch facilities. Payload processing handled by private firms also started to occur outside of KSC. Reagan's 1988 space policy furthered the movement of this work from KSC to commercial companies. That same year, launch complexes on Cape Canaveral Air Force Force Station started transferring from NASA to Air Force Space Command management.
In the 1990s, though KSC was not performing the hands-on ELV work, engineers still maintained an understanding of ELVs and had contracts allowing them insight into the vehicles so they could provide knowledgeable oversight. KSC also worked on ELV research and analysis and the contractors were able to utilize KSC personnel as a resource for technical issues. KSC, with the payload and launch vehicle industries, developed advances in automation of the ELV launch and ground operations to enable competitiveness of U.S. rockets against the global market.
In 1998, the Launch Services Program (LSP) formed at KSC, pulling together programs (and personnel) that already existed at KSC, GRC, Goddard Space Flight Center, and more to manage the launch of NASA and NOAA robotic missions. Cape Canaveral Space Force Station and VAFB are the primary launch sites for LSP missions, though other sites are occasionally used. LSP payloads such as the Mars Science Laboratory have been processed at KSC before being transferred to a launch pad on Cape Canaveral Space Force Station.
On 16 November 2022, at 06:47:44 UTC the Space Launch System (SLS) was launched from Complex 39B as part of the Artemis 1 mission.
As the International Space Station modules design began in the early 1990s, KSC began to work with other NASA centers and international partners to prepare for processing before launch onboard the Space Shuttles. KSC utilized its hands-on experience processing the 22 Spacelab missions in the Operations and Checkout Building to gather expectations of ISS processing. These experiences were incorporated into the design of the Space Station Processing Facility (SSPF), which began construction in 1991. The Space Station Directorate formed in 1996. KSC personnel were embedded at station module factories for insight into their processes.
From 1997 to 2007, KSC planned and performed on the ground integration tests and checkouts of station modules: three Multi-Element Integration Testing (MEIT) sessions and the Integration Systems Test (IST). Numerous issues were found and corrected that would have been difficult to nearly impossible to do on-orbit.
Today KSC continues to process ISS payloads from across the world before launch along with developing its experiments for on orbit. The proposed Lunar Gateway would be manufactured and processed at the Space Station Processing Facility.
The following are current programs and initiatives at Kennedy Space Center:
Commercial Crew Program
Exploration Ground Systems Program
NASA is currently designing the next heavy launch vehicle known as the Space Launch System (SLS) for continuation of human spaceflight.
On December 5, 2014, NASA launched the first uncrewed flight test of the Orion Multi-Purpose Crew Vehicle (MPCV), currently under development to facilitate human exploration of the Moon and Mars.
Launch Services Program
Educational Launch of Nanosatellites (ELaNa)
Research and Technology
Artemis program
Lunar Gateway
International Space Station Payloads
Camp KSC: educational camps for schoolchildren in spring and summer, with a focus on space, aviation and robotics.
The KSC Industrial Area, where many of the center's support facilities are located, is 5 miles (8 km) south of LC-39. It includes the Headquarters Building, the Operations and Checkout Building and the Central Instrumentation Facility. The astronaut crew quarters are in the O&C; before it was completed, the astronaut crew quarters were located in Hangar S at the Cape Canaveral Missile Test Annex (now Cape Canaveral Space Force Station). Located at KSC was the Merritt Island Spaceflight Tracking and Data Network station (MILA), a key radio communications and spacecraft tracking complex.
Facilities at the Kennedy Space Center are directly related to its mission to launch and recover missions. Facilities are available to prepare and maintain spacecraft and payloads for flight. The Headquarters (HQ) Building houses offices for the Center Director, library, film and photo archives, a print shop and security. When the KSC Library first opened, it was part of the Army Ballistic Missile Agency. However, in 1965, the library moved into three separate sections in the newly opened NASA headquarters before eventually becoming a single unit in 1970. The library contains over four million items related to the history and the work at Kennedy. As one of ten NASA center libraries in the country, their collection focuses on engineering, science, and technology. The archives contain planning documents, film reels, and original photographs covering the history of KSC. The library is not open to the public but is available for KSC, Space Force, and Navy employees who work on site. Many of the media items from the collection are digitized and available through NASA's KSC Media Gallery Archived December 6, 2020, at the Wayback Machine or through their more up-to-date Flickr gallery.
A new Headquarters Building was completed in 2019 as part of the Central Campus consolidation. Groundbreaking began in 2014.
The center operated its own 17-mile (27 km) short-line railroad. This operation was discontinued in 2015, with the sale of its final two locomotives. A third had already been donated to a museum. The line was costing $1.3 million annually to maintain.
The Neil Armstrong Operations and Checkout Building (O&C) (previously known as the Manned Spacecraft Operations Building) is a historic site on the U.S. National Register of Historic Places dating back to the 1960s and was used to receive, process, and integrate payloads for the Gemini and Apollo programs, the Skylab program in the 1970s, and for initial segments of the International Space Station through the 1990s. The Apollo and Space Shuttle astronauts would board the astronaut transfer van to launch complex 39 from the O&C building.
The three-story, 457,000-square-foot (42,500 m2) Space Station Processing Facility (SSPF) consists of two enormous processing bays, an airlock, operational control rooms, laboratories, logistics areas and office space for support of non-hazardous Space Station and Shuttle payloads to ISO 14644-1 class 5 standards. Opened in 1994, it is the largest factory building in the KSC industrial area.
The Vertical Processing Facility (VPF) features a 71-by-38-foot (22 by 12 m) door where payloads that are processed in the vertical position are brought in and manipulated with two overhead cranes and a hoist capable of lifting up to 35 short tons (32 t).
The Hypergolic Maintenance and Checkout Area (HMCA) comprises three buildings that are isolated from the rest of the industrial area because of the hazardous materials handled there. Hypergolic-fueled modules that made up the Space Shuttle Orbiter's reaction control system, orbital maneuvering system and auxiliary power units were stored and serviced in the HMCF.
The Multi-Payload Processing Facility is a 19,647 square feet (1,825.3 m2) building used for Orion spacecraft and payload processing.
The Payload Hazardous Servicing Facility (PHSF) contains a 70-by-110-foot (21 by 34 m) service bay, with a 100,000-pound (45,000 kg), 85-foot (26 m) hook height. It also contains a 58-by-80-foot (18 by 24 m) payload airlock. Its temperature is maintained at 70 °F (21 °C).[55]
The Blue Origin rocket manufacturing facility is located immediately south of the KSC visitor complex. Completed in 2019, it serves as the company's factory for the manufacture of New Glenn orbital rockets.
Launch Complex 39 (LC-39) was originally built for the Saturn V, the largest and most powerful operational launch vehicle until the Space Launch System, for the Apollo crewed Moon landing program. Since the end of the Apollo program in 1972, LC-39 has been used to launch every NASA human space flight, including Skylab (1973), the Apollo–Soyuz Test Project (1975), and the Space Shuttle program (1981–2011).
Since December 1968, all launch operations have been conducted from launch pads A and B at LC-39. Both pads are on the ocean, 3 miles (4.8 km) east of the VAB. From 1969 to 1972, LC-39 was the "Moonport" for all six Apollo crewed Moon landing missions using the Saturn V, and was used from 1981 to 2011 for all Space Shuttle launches.
Human missions to the Moon required the large three-stage Saturn V rocket, which was 363 feet (111 meters) tall and 33 feet (10 meters) in diameter. At KSC, Launch Complex 39 was built on Merritt Island to accommodate the new rocket. Construction of the $800 million project began in November 1962. LC-39 pads A and B were completed by October 1965 (planned Pads C, D and E were canceled), the VAB was completed in June 1965, and the infrastructure by late 1966.
The complex includes: the Vehicle Assembly Building (VAB), a 130,000,000 cubic feet (3,700,000 m3) hangar capable of holding four Saturn Vs. The VAB was the largest structure in the world by volume when completed in 1965.
a transporter capable of carrying 5,440 tons along a crawlerway to either of two launch pads;
a 446-foot (136 m) mobile service structure, with three Mobile Launcher Platforms, each containing a fixed launch umbilical tower;
the Launch Control Center; and
a news media facility.
Launch Complex 48 (LC-48) is a multi-user launch site under construction for small launchers and spacecraft. It will be located between Launch Complex 39A and Space Launch Complex 41, with LC-39A to the north and SLC-41 to the south. LC-48 will be constructed as a "clean pad" to support multiple launch systems with differing propellant needs. While initially only planned to have a single pad, the complex is capable of being expanded to two at a later date.
As a part of promoting commercial space industry growth in the area and the overall center as a multi-user spaceport, KSC leases some of its properties. Here are some major examples:
Exploration Park to multiple users (partnership with Space Florida)
Shuttle Landing Facility to Space Florida (who contracts use to private companies)
Orbiter Processing Facility (OPF)-3 to Boeing (for CST-100 Starliner)
Launch Complex 39A, Launch Control Center Firing Room 4 and land for SpaceX's Roberts Road facility (Hanger X) to SpaceX
O&C High Bay to Lockheed Martin (for Orion processing)
Land for FPL's Space Coast Next Generation Solar Energy Center to Florida Power and Light (FPL)
Hypergolic Maintenance Facility (HMF) to United Paradyne Corporation (UPC)
The Kennedy Space Center Visitor Complex, operated by Delaware North since 1995, has a variety of exhibits, artifacts, displays and attractions on the history and future of human and robotic spaceflight. Bus tours of KSC originate from here. The complex also includes the separate Apollo/Saturn V Center, north of the VAB and the United States Astronaut Hall of Fame, six miles west near Titusville. There were 1.5 million visitors in 2009. It had some 700 employees.
It was announced on May 29, 2015, that the Astronaut Hall of Fame exhibit would be moved from its current location to another location within the Visitor Complex to make room for an upcoming high-tech attraction entitled "Heroes and Legends". The attraction, designed by Orlando-based design firm Falcon's Treehouse, opened November 11, 2016.
In March 2016, the visitor center unveiled the new location of the iconic countdown clock at the complex's entrance; previously, the clock was located with a flagpole at the press site. The clock was originally built and installed in 1969 and listed with the flagpole in the National Register of Historic Places in January 2000. In 2019, NASA celebrated the 50th anniversary of the Apollo program, and the launch of Apollo 10 on May 18. In summer of 2019, Lunar Module 9 (LM-9) was relocated to the Apollo/Saturn V Center as part of an initiative to rededicate the center and celebrate the 50th anniversary of the Apollo Program.
Historic locations
NASA lists the following Historic Districts at KSC; each district has multiple associated facilities:
Launch Complex 39: Pad A Historic District
Launch Complex 39: Pad B Historic District
Shuttle Landing Facility (SLF) Area Historic District
Orbiter Processing Historic District
Solid Rocket Booster (SRB) Disassembly and Refurbishment Complex Historic District
NASA KSC Railroad System Historic District
NASA-owned Cape Canaveral Space Force Station Industrial Area Historic District
There are 24 historic properties outside of these historic districts, including the Space Shuttle Atlantis, Vehicle Assembly Building, Crawlerway, and Operations and Checkout Building.[71] KSC has one National Historic Landmark, 78 National Register of Historic Places (NRHP) listed or eligible sites, and 100 Archaeological Sites.
Further information: John F. Kennedy Space Center MPS
Other facilities
The Rotation, Processing and Surge Facility (RPSF) is responsible for the preparation of solid rocket booster segments for transportation to the Vehicle Assembly Building (VAB). The RPSF was built in 1984 to perform SRB operations that had previously been conducted in high bays 2 and 4 of the VAB at the beginning of the Space Shuttle program. It was used until the Space Shuttle's retirement, and will be used in the future by the Space Launch System[75] (SLS) and OmegA rockets.
In the heart of Old Town, historic factory is among the oldest in Grasse ... Indeed the current premises sheltered from their beginning in 1782, a perfume factory. In 1926, after the famous painter Jean Honoré Fragonard, it takes the name of Parfumerie Fragonard. Since then, every day, we produce are our perfumes, cosmetics and soaps in a respectful environment of tradition. We would be happy to welcome you and offer you a guided tour during which you will discover the different manufacturing processes and packaging our products. At the end of your visit, you can admire 3000 years of history of perfume through our private museum.
Dedicated to the perfume and aromatic plants, Flower Factory is surrounded by a beautiful garden scented plants ... the gates of Grasse, this contemporary factory opened in 1986 is equipped with very modern machinery for the manufacture and packaging of our products.
WORKSHOP ODOR "Perfumer's Apprentice"
Available on the French Riviera and Paris, in factories, workshops Perfumers Apprentice can discover the expertise of Perfumer: the history of perfume, raw materials and different extraction methods.
Experience unforgettable sense centered on the composition of a toilet water (100 ml) in aromatic notes of citrus and orange blossom, by assembling the different species made available. A fun and exciting experience in the world of perfumery, which proposes the course led by the teacher, the bottle and its bag, apron "apprentice" printed Fragonard, the diploma signed by the teacher and the summary of the composition .
One of our guides will accompany you as a result of the workshop for a visit "Prestige" from our factory.
Located in one of the oldest houses in the historic center of the city, this perfume offers original creations of Didier Gaglewski.
Didier Gaglewski, "nose" in Grasse, began offering its achievements in the framework Living in Provence and in Paris, Germany and Switzerland. Both "artisan", "artist", he decided to offer his achievements directly driven by the idea that the quality, originality and respect perfume composition will dress with fun, humor and quality its customers.
Requiring each of its perfumes, made in the privacy of his laboratory, took several months of research. In partnership with Michelle Cavalier and the "garden of La Bastide," Didier Gaglewski also remains closer to the flowers and working the land. Try to trace extraction techniques inherited from the past and plants specific to the region perfumes seduce and make a very personal and authentic. This atypical creator is distinguished by its compositions made in Grasse basin, its choice to favor natural raw materials and the search for sobriety.
Front satisfaction and customer demands wishing to regain the proposed perfumes, shop in Grasse, 12 rue of the Oratory, just steps from the International Perfume Museum to discover the scents and recent creations.
The country house of Aromas
Based in Saint Cézaire on Siagne in the Pays de Grasse, the Bastide aromas manufactures and packages fragrances since 1995.
Saint Cézaire on Siagne is a typical Provencal village a few kilometers from Grasse, the world capital of perfumery.
The homemade studio human scale can meet all your demands. The 100% handmade is carried out in the workshop without intermediary, under the control of a chemist.
La Bastide des Aromas, respects the traditions of the Grasse region and offers the exclusive fragrances custom made in the workshop on-site, high quality, with particular stress on the fragrance concentration, her outfit and originality.