View allAll Photos Tagged Configuration
Mabuti at ginawang airconary itong BF106 ni Magicline dahil mukhang sa 2020, wala na dapat non-AC buses sa EDSA.
Company/Owner: Magicline Express Corporation
Fleet/Bus Number: 8885888
Classification: Non-Air-conditioned/Air-conditioned City Bus
Coachbuilder: Santarosa Motor Works, Inc. / Columbian Motors Corporation (rebody); Aspire Manufacturing and Rebuilding (original)
Body Model: Santarosa Daewoo Bus BF106
Original Body Model: Daewoo/Aspire HFC6108H Imperial Series
Engine Model: Doosan DE08TIS
Chassis Model: Daewoo BF106 (KL5UK42HD3P)
Transmission: 6-speed Manual Transmission
Suspension: Leaf Spring Suspension
Seating Configuration: 3×2
Seating Capacity: 58
Franchise route: Grotto (SJDM Bulacan)–NAIA via EDSA, SM Fairview
Route: Ninoy Aquino International Airport, Pasay City/Parañaque City–Sapang Palay, San Jose Del Monte City, Bulacan via N195 (Ninoy Aquino Avenue) / N194 (NAIA Road) / N61 (Roxas Boulevard)/EDSA/ N174 (East Avenue) / N170 [Commonwealth Avenue (Quezon City)] / N127 (Quirino Highway) and vice versa
Areas passing (underlines are designated stops for this bus scheme - EDSA area only: Magallanes–Ermin Garcia Avenue): Tambo\Coastal Mall\Bayview International Towers\City of Dreams\Airport Road\Baclaran Church\The Heritage Hotel\F.B. Harrison Street\Pasay Rotonda/Metro Point Mall\Tramo\Malibay/Cabrera\Evangelista\Magallanes\Ayala Avenue\Buendia Avenue\Estrella\Guadalupe\Boni/Pioneer\Reliance\Shaw Boulevard\SM Megamall\Ortigas Avenue\Robinsons Galleria\Boni Serrano\Main Avenue\Araneta Center Cubao/Farmers\Baliwag Transit/Five Star\Ermin Garcia Avenue\LTFRB Central Office/LTO Central Office\NIA Road\V. Luna Avenue/Land Registration Authority East Ave\Philippine Statistics Authority\SSS East Ave/BSP East Ave\BIR Road\East Avenue Medical Center\Philippine Heart Center\Matalino Street/Nat'l Kidney Transplant Institute\Quezon Memorial Circle/City Hall Gate 10\Nat'l Housing Authority Main Office/Maharlika Street\Philcoa\Techno Hub\Central Avenue\INC Templo Central\Tandang Sora Avenue\Luzon Avenue\Diliman Doctors Hospital\Don Antonio\Ever Gotesco\Saint Peter Parish\Sandiganbayan\Commission on Audit\Commonwealth Market\Manggahan\INC Capitol\Litex\Don Fabian\Doña Carmen Avenue\Winston Street\Pearl Drive\Fairview Center Mall/NCBA Fairview\Our Lady of Fatima Regalado\AMA Fairview/Bristol Street\Mindanao-Jollibee\Brittany Square/Belfast\Commonwealth Hospital and Medical Center\SM City Fairview\Trees Residences\Hilltop Mansion Subdivision/Our Lady of Fatima Hilltop\Mater Carmeli School\Sacred Heart Novitiate\Quezon City–Caloocan Boundary\Sacred Heart Village/Dela Costa Homes 2\Midway Park Subdivision\Amparo Subdivision Gate 2\Guadanoville Subdivision\Mountain Heights Subdivision\Pangarap Village\Bankers Village 2/North Caloocan Doctors Hospital\Cefels Park 3 Subdivision\Malaria Road\Funnside Ningnangan Caloocan\Ascoville Road\Sampaguita Street\Altaraza Town Center/Pleasant Hills Subdivision\Diamond Crest Village\Savano Park\Pecsonville Subdivision/SM Tungko (SM San Jose del Monte)\Skyline Hospital\Gumaok East\Francisco Homes Subdivision\Starmall San Jose del Monte\Palmera Subdivision\Igay Road\Curva\Classica Northgate\Santo Cristo\Tialo Bridge\Towerville\Newtown\Road 1\Bestlink College SJDM/Quarry\Road 2 (Dr. E. V. Roquero, Sr. Road)\Road 5\Minuyan\Citrus Road\Santo Niño I\Lawang Pari\Santo Niño II/Block 64 Street\Assumption\Libis-Rancho\Kadiwa/Sampol
Type of Operation: City Operation Public Utility Bus (Bus Segregation A | Regular Class/Economy Class)
Area of Operations: Central Luzon (Region III)/National Capital Region (NCR)
Shot Location: EDSA-Shaw, Mandaluyong City
Date Taken: May 12, 2018
Notices:
* Please DON'T GRAB A PHOTO WITHOUT A PERMISSION. If you're going to GRAB IT, please give A CREDIT TO THE OWNER. Also, don't PRINT SCREEN my photos.
** If I have mistakes on the specifications, please comment in a good manner so that I can edit it immediately.
*** The specifications and routes (for provincial, inter-provincial, and city operation) mentioned above are subjected for verification and may be changed without prior notice.
**** The vehicle's registration plate(s), conduction sticker(s), and/or persons (if applicable) were pixelated/blurred to prevent any conflict with the photographer, the bus company and/or to the car owner for their security and/or privacy purposes. So, don't use their plate number, conduction sticker, and vehicle tag as an evidence for any incident. And, I have taken this photo for bus fanatics, bus enthusiasts, and bus lovers purposes.
Company/Owner: Golden Bee Transport and Logistics Corporation
Fleet/Bus Number: 972
Classification: Air-conditioned Provincial Bus
Coachbuilder: Santarosa Motor Works, Inc./Columbian Manufacturing Corporation
Body Model: Daewoo/Santarosa BS106
Engine Model: Doosan DE08TIS
Chassis Model: Daewoo BS106 (PL5UM52HDEK)
Transmission: Manual (6-speed forward, 1-speed reverse)
Suspension: Leaf Spring Suspension
Seating Configuration: 3×2
Seating Capacity: 61
Route: Baliuag, Bulacan–Cubao, Quezon City via Old Cagayan Valley Road / Highway 1 (Doña Remedios Trinidad Highway)
Municipalities/cities passing: Pulilan/Plaridel/Guiguinto
Type of Operation: Provincial Operation Public Utility Bus (Regular Class)
Area of Operation: Central Luzon (Region III)
Shot Location: Pulilan Regional Road (Old Cagayan Valley Road), Barangay Cut-cot, Pulilan, Bulacan
Date Taken: October 5, 2015
Notices:
* Please DON'T GRAB A PHOTO WITHOUT A PERMISSION. If you're going to GRAB IT, please give A CREDIT TO THE OWNER. Also, don't PRINT SCREEN my photos.
** If I have mistakes on the specifications, please comment in a good manner so that I can edit it immediately.
*** The specifications and routes (for provincial, inter-provincial, and city operation) mentioned above are subjected for verification and may be changed without prior notice.
**** The vehicle's registration plate(s), conduction sticker(s), and/or persons (if applicable) were pixelated/blurred to prevent any conflict with the photographer, the bus company and/or to the car owner for their security and/or privacy purposes. So, don't use their plate number, conduction sticker, and vehicle tag as an evidence for any incident. And, I have taken this photo for bus fanatics, bus enthusiasts, and bus lovers purposes.
Flammable Tanker
Truck Manufacturer: MAN Truck & Bus AG
Model: MAN TGS
Trailer: 3 Axle Flammable Tanker Trailer
Chassis 33.360
Engine:
Suspension:
Axle Configuration: 6x4
Shot Location: Mindanao Ave
Flammable Tanker
Truck Manufacturer: MAN Truck & Bus AG
Model: CLA
Chassis: 26.280
Engine:
Suspension:
Axle Configuration: 6x4
Shot Location: A.boni
www.ravishlondon.com/londonstreetart
Together Shoreditch and Spitalfields in the East of London constitute the most exciting place to be in London. The population is young, dynamic and imaginative; Friday and Saturday nights are a riot with a plethora of bars and clubs many with their own unique flavour. But what makes this area really special is that Shoreditch and Spitalfields comprise what one might call, ‘the square mile of art’; a de factor open air art gallery; with graffiti, posters and paste-ups being displayed on the main streets, down the side roads and in all the nooks and crannies of this post-industrial environ.
From Eine’s huge single letters being painted on shop shutters, to the haunting propaganda posters of Obey, to Cartrain’s political black and white pop-art; and to the one very small bronze coloured plastic circle, with the imprint of a dog shit and a man's foot about to step into it, which I once saw pasted to a wall, there is an incredible diversity.
Being on the streets, the work can be destroyed, taken or painted over at any minute. It is fragile and transient. Furthermore the juxtaposition of different pieces of art is random and unpredictable both in content and its location, which means that each day throws up a new and unique configuration of work within the streets, which you can only experience by travelling through the city.
Street Art Beginnings
The reasons for why East London has seen the flowering of street art are manifold. The post-industrial legacy of Shoreditch’s crumbling low-rise warehouses, not only provides an environment in which the artists and designers can do their work, but East London’s proximity to the City of London provides an economic source of support for the artists and designers; and finally Shoreditch with its building sites, old dilapidated warehouses provides a canvas upon which those artists can display their work and increase their commercial value.
Set against the characterless nature of the steely post-modernity of the city, the autumnal colours of the terraced warehouses in Shoreditch, no bigger than four to five stories high; offer a reminder of the legacy of a thriving fabrics and furniture industry which blossomed in the seventeenth Century. Both Shoreditch and Spitalfields have industrial pasts linked to the textiles industry, which fell into terminal decline by the twentieth century and was almost non-existent by the end of Wolrd War II. The decline was mirrored in the many three to four storey warehouses that were left to decay.
The general decline was arrested in the 1980s with the emergence of Shoreditch and Hoxton (Hoxton and Shoreditch are used interchandeably to refer to the same area) as a centre for new artists. It is difficult to say what attracted the artists to this area. But it was likely to be a combination of the spaces offered by the old warehouses, the cheap rents, and the location of Shoreditch and Spitalfields close to the City of London; where the money was to buy and fund artistic endeavour.
Not just that but post-war Shoreditch dominated by tens of post-war tower blocks, built amidst the ruins of the terraced housing that lay there before, which was bombed during World War II; had the rough edge which might inspire an artist. Shoreditch hums with the industry of newly arrived immigrants but also of the dangers of the poorer communities which inhabit these areas. Homeless people can be found sat underneath bridges on the main thoroughfares on Friday and Saturday nights; and Shoreditch is apparently home to one of the largest concentrations of striptease joints and a number of prostitutes. So, Shoreditch is a crumbling dirty, dodgy, polluted mess but it also has money; and these two factors provide an intoxicating mix for artists, who can take inspiration from their environment, but also rub shoulders with people who have the kind of money to buy their work.
By the early nineties Hoxton’s reputation as a centre for artists had become well established. As Jess Cartner-Morley puts it ‘Hoxton was invented in 1993. Before that, there was only 'Oxton, a scruffy no man's land of pie and mash and cheap market-stall clothing…’ At that time artists like Damien Hirst and Tracy Emin were taking part in ‘A Fete Worth than Death’ an arts based event in Hoxton. Gradually these artists began to create their own gravity, attracting more and more of their own like. Clubs and bars began to emerge, as did a Hoxton style, ‘the Hoxton fin’ being a trademark haircut. Many designers and artists located around Shoreditch and Spitalfields. Shoreditch has also become a hive of studios for artists, vintage fashion shops, art students and musicians.
At the same time as an artistic community was forming fuelled by money from the City, London was subject to a revolution in street art. According to Ward, writing for Time Out, the street art scene began in the mid-1980s as part of London’s hip-hop scene. Graffiti artists, emulating what was going on Stateside, began to tag their names all over London. According to Ward many of those pioneers ‘went on to paint legal commissions and are at the heart of today’s scene’. That is to say, from the community of artists congregating in East London, a number were inspired by graffiti, and because the East London, with its countless dilapidated warehouses, and building sites, offered such a good canvas; they went on to use the East London as a canvas for their work.
Little seems to have been written about the individual journey’s particular street artists have taken to get to where they are, which help illuminate some of the issues talked about in this section. Cartrain said that Banksy was a huge influence for him commenting that, "I've sent him a few emails showing him my work and he sent me a signed piece of his work in the post."
What created the East London street art scene may also kill it
The East London urban art scene is unlikely to last forever, being the symptom of a delicate juxtaposition of industrial decline and economic forces.
The irony is that the same factors which are responsible for the creation of the East London art scene are likely to destroy it.
Politicians from all parties, spiritual leaders for global capital, tell us of the unstoppable forces of globalisation. They say if Britain is to continue to dip its paw into the cream of the world’s wealth it needs to become a post-industrial service economy; suggesting a rosy future of millions of Asians slaving away co-ordinated by keyboard tapping British suits, feet on desk, leant back on high backed leather chairs, secretary blowing them off.
Art, which is feeble and dependent upon the financial growth of an economy for its survival, will have to shape itself around the needs and demands of capital.
The financial district of the City of London, lying to the south of Shoreditch, has been successfully promoted as a global financial centre, and its mighty power is slowly expanding its way northwards. Plans are afoot for the glass foot soldiers of mammon, fuelled by speculative property investment, to gradually advance northwards, replacing old warehouses with a caravan of Starbucks and Japanese sushi places and a concomitant reduction in dead spaces to portray the art, increased security to capture and ward off street artists, increased property prices and the eventual eviction of the artistic community. Spitalfields has already had big corporate sized chunks taken out of it, with one half of the old Spitalfields Market being sacrificed for corporate interests in the last five years.
So then the very same financial forces, and post-industrial legacy, which have worked to create this micro-environment for street art to thrive, are the same forces which will in time eventually destroy it. Maybe the community will move northwards, maybe it will dissipate, but until that moment lets just enjoy what the community puts out there, for its own financial interests, for their own ego and also, just maybe, for the benefit of the people.
Banksy
Banksy is the street artist par excellence. London’s street art scene is vibrant and diverse. There is some good, cure, kitschy stuff out there, but in terms of creativity and imagination Banksy leads by a city mile. His stuff is invariably shocking, funny, thought provoking and challenging.
Banksy considers himself to be a graffiti artist, which is what he grew up doing in the Bristol area in the late eighties. According to Hattenstone (2003) Banksy, who was expelled from his school, and who spent some time in prison for petty crimes, started graffiti at the age of 14, quickly switching over to stencils, which he uses today, because he didn’t find he had a particular talent for the former. His work today involves a mixture of graffiti and stencils although he has shown a capacity for using a multitude of materials.
Key works in London have included:
•In London Zoo he climbed into the penguin enclosure and painted "We're bored of fish" in six-foot-high letters.
•
•In 2004 he placed a dead rat in a glass-fronted box, and stuck the box on a wall of the Natural History Museum.
•
•‘A designated riot area’ at the bottom of Nelson’s Column.
•
•He placed a painting called Early Man Goes to Market, with a human figure hunting wildlife while pushing a shopping trolley, in the British Museum.
•
His work seems to be driven by an insatiable desire to go on producing. In an interview with Shepherd Fairey he said, ‘Anything that stands in the way of achieving that piece is the enemy, whether it’s your mum, the cops, someone telling you that you sold out, or someone saying, "Let’s just stay in tonight and get pizza." Banksy gives the impression of being a person in the mould of Tiger Woods, Michael Schumacher or Lance Armstrong. Someone with undoubted talent and yet a true workaholic dedicated to his chosen profession.
Its also driven by the buzz of ‘getting away with it’. He said to Hattenstone, ‘The art to it is not getting picked up for it, and that's the biggest buzz at the end of the day because you could stick all my shit in Tate Modern and have an opening with Tony Blair and Kate Moss on roller blades handing out vol-au-vents and it wouldn't be as exciting as it is when you go out and you paint something big where you shouldn't do. The feeling you get when you sit home on the sofa at the end of that, having a fag and thinking there's no way they're going to rumble me, it's amazing... better than sex, better than drugs, the buzz.’
Whilst Banksy has preferred to remain anonymous he does provide a website and does the occasional interview putting his work in context (see the Fairey interview).
Banksy’s anonymity is very important to him. Simon Hattenstone, who interviewed Banksy in 2003, said it was because graffiti was illegal, which makes Banksy a criminal. Banksy has not spoken directly on why he wishes to maintain his anonymity. It is clear that Banksy despises the notion of fame. The irony of course is that ‘Banksy’ the brand is far from being anonymous, given that the artist uses it on most if not all of his work. In using this brand name Banksy helps fulfil the need, which fuels a lot of graffiti artists, of wanting to be recognised, the need of ego.
Banksy is not against using his work to ‘pay the bills’ as he puts it. He has for example designed the cover of a Blur album, although he has pledged never to do a commercial job again, as a means of protecting his anonymity. Nevertheless he continues to produce limited edition pieces, which sell in galleries usually for prices, which give him a bit of spending money after he has paid the bills. Banksy has said, ‘If it’s something you actually believe in, doing something commercial doesn’t turn it to shit just because it’s commercial’ (Fairey, 2008). Banksy has over time passed from urban street artist into international artistic superstar, albeit an anonymous one.
Banksy has a definite concern for the oppressed in society. He often does small stencils of despised rats and ridiculous monkeys with signs saying things to the effect of ‘laugh now but one day we’ll be in charge’. Whilst some seem to read into this that Banksy is trying to ferment a revolutionary zeal in the dispossessed, such that one day they will rise up and slit the throats of the powers that be, so far his concern seems no more and no less than just a genuine human concern for the oppressed. Some of what seems to fuel his work is not so much his hatred of the system but at being at the bottom of it. He said to Hattenstone (2003) ‘Yeah, it's all about retribution really… Just doing a tag is about retribution. If you don't own a train company then you go and paint on one instead. It all comes from that thing at school when you had to have name tags in the back of something - that makes it belong to you. You can own half the city by scribbling your name over it’
Charlie Brooker of the Guardian has criticised Banksy for his depictions of a monkey wearing a sandwich board with 'lying to the police is never wrong' written on it. Certainly such a black and white statement seems out of kilter with more balanced assessments that Banksy has made. Brooker challenges Banksy asking whether Ian Huntley would have been right to have lied to the police?
Brooker has also criticized Banksy for the seemingly meaninglessness of some of this images. Brooker says, ‘Take his political stuff. One featured that Vietnamese girl who had her clothes napalmed off. Ho-hum, a familiar image, you think. I'll just be on my way to my 9 to 5 desk job, mindless drone that I am. Then, with an astonished lurch, you notice sly, subversive genius Banksy has stencilled Mickey Mouse and Ronald McDonald either side of her. Wham! The message hits you like a lead bus: America ... um ... war ... er ... Disney ... and stuff.’ Brooker has seemingly oversimplified Banksy’s message, if indeed Banksy has one, to fuel his own criticisms. It is easy to see that for many the Vietnam painting tells us that the United States likes to represent itself with happy smiling characters, that hide the effects of its nefarious activities responsible for the real life faces of distress seen on the young girl. Something that we should be constantly reminded of. But then that’s a matter of politics not of meaninglessness.
Banksy’s ingenuity comes through in his philosophy on progression, ‘I’m always trying to move on’ he says. In the interview he gave with Shepherd Fairey he explained that he has started reinvesting his money in to new more ambitious projects which have involved putting scaffolding put up against buildings, covering the scaffolding with plastic sheeting and then using the cover of the sheets to do his paintings unnoticed.
Banksy has balls. Outside of London he has painted images in Disney Land; and on the Israeli wall surrounding Palestine. How far is he willing to push it? What about trying something at the headquarters of the BNP, or on army barracks, or at a brothel or strip club employing sex slaves, or playing around with corporate advertising a la Adbusters?
This configuration with a Sony A7S and 3-axis brushless gimbal weighs about 4.8 kg and is able to fly about 12 minutes for aerial video footage.
Commentary.
Ocean, land, harbour – an unusual configuration.
The geology of south-west Argyll provides a series of land-protected harbours and ideal sailing waters.
Therefore, this ancient but mellow coastline of Dalriada is a mecca for yachting marinas.
In this scene, looking west, Tayvallich is one of very few east-facing villages on the majestic western seaboard.
A strip of land shelters the multifarious blue, yellow, white and red craft from the Atlantic elements.
Uncommercialised, unspoilt Tayvallich in early morning reflects the land and water dwellings in a crystal-clear symmetry.
Loch Melfort, Crinan, Tayvallich, Ardfern and Craobh Haven. Hidden jewels in an immensely fractured, twisting and convoluted coastline.
With island vistas and visits to Islay, Jura, Scarba, Luing, Seil, Kerrera and Lismore these cosy, calm and peaceful harbours
act as perfect sanctuaries to the incredible sea-kingdom of Dalriada.
NSP Luxury Coach
Bus Number: 168-21
Body: Xiamen King Long United (King Long)
Model: King Long XMQ6123Y
Chassis: King Long XMQ6121R6 (LA6R1HS)
Engine: Cummins C300-20
Suspension
Seating Configuration: 2x2
Capacity
Shot Location: Shell Station, Balintawak
Solid North Transit Inc.
Bus number: 1629
Area of Operation: Provincial Operation
Seating Configuration: 2x2
Seating Capacity: 45+1
Bus Manufacturer: Zhengzhou Yutong Bus Co., Ltd.
Model: ZK6107HA
Chassis: Yutong ZK6107CRA
Engine: Yuchai YC6A260-30
Suspension: Air Suspension
Shot Location: North EDSA
Nang mawala ang PSY (Pasay)–TUG (Tuguegarao) ni Victory, gumawa sila nang paraan kung paano pa rin nila mapapatakbo ang PSY–TUG.
Company/Owner: Victory Liner, Inc.
Fleet/Bus Number: 6020
Classification: Air-conditioned Provincial Bus
Coachbuilder: Santarosa Motor Works, Inc./Columbian Motors Corporation
Body Model: Nissan Diesel/Santarosa EXFOH
Engine Model: Nissan Diesel PF6-TA (PF6-A)
Chassis Model: Nissan Diesel JA450SSN
Transmission: 6-speed Manual Transmission
Suspension: Leaf Spring Suspension
Seating Configuration: 2×2
Seating Capacity: 49
Franchise route: Tuguegarao City (Cagayan)–Manila
Route: Tuguegarao City, Cagayan [TUG, CV]–San Fernando City, Pampanga [SFP, PP]–Pasay City [PSY] via N1 (Maharlika Highway) / N114 (Pangasinan–Nueva Ecija Road) / Pura–Guimba Road / E1 [TPLEX-Pura–SCTEX-Amucao–NLEX-SCTEX Connector; NLEX-Dau–NLEX-San Fernando/Robinsons Starmills–NLEX-Balintawak] / N215 (Dau Access Road)
Municipalities/cities passing: Peñablanca/San Pablo/Cabagan/Tumauini/Ilagan City [ILA]/Gamu/Naguilian/Reina Mercedes/Cauayan City [CYZ]/Alicia/Echague/San Isidro/Santiago City [STO]/Cordon/Diadi/Bagabag/Solano [SOL]/Bayombong/Bambang [BBM]/Ineangan (Dupax del Norte)/Gabut (Dupax del Sur)/Aritao [ART]/Santa Fe/Carranglan/San Jose City [SJC]/Science City of Muñoz/Talavera/Santo Domingo/Guimba [GUI]/Pura–Dau (Mabalacat City) [DAU]–San Fernando City [SFP]
Type of Operation: Provincial Operation Public Utility Bus (Regular Class)
Area of Operation: Cagayan Valley (Region II)
Shot Location: Miranda Boulevard, Barangay Calao East, Santiago City, Isabela
Date Taken: May 18, 2018 (15:06H)
Notices:
* Please DON'T GRAB A PHOTO WITHOUT A PERMISSION. If you're going to GRAB IT, please give A CREDIT TO THE OWNER. Also, don't PRINT SCREEN my photos.
** If I have mistakes on the specifications, please comment in a good manner so that I can edit it immediately.
*** The specifications and routes (for provincial, inter-provincial, and city operation) mentioned above are subjected for verification and may be changed without prior notice.
**** The vehicle's registration plate(s), conduction sticker(s), and/or persons (if applicable) were pixelated/blurred to prevent any conflict with the photographer, the bus company and/or to the car owner for their security and/or privacy purposes. So, don't use their plate number, conduction sticker, and vehicle tag as an evidence for any incident. And, I have taken this photo for bus fanatics, bus enthusiasts, and bus lovers purposes.
Company/Owner: Gold Line Tours, Inc.
Fleet/Bus Number: 637
Classification: Air-conditioned Tourist Chartered Bus
Coachbuilder: Del Monte Motor Works, Inc.
Body Model: Mercedes-Benz/Del Monte Aero Adamant OH 1625
Engine Model: Mercedes-Benz OM 449 LA
Chassis Model: Mercedes-Benz OH1625L
Transmission: 6-speed Manual Transmission
Suspension: Air Suspension
Seating Configuration: 2×2
Seating Capacity: 40
Franchise route: Manila to any point of the Philippines
Route: various (Tourist Chartered)
Municipalities/cities passing: N/A
Type of Operation: Tourist Operation Non-Public Utility Bus (Special Trip/Tourist Class)
Area of Operation: Any point of Philippines: Ilocos Region (Region I), Cagayan Valley (Region II), Central Luzon (Region III), CALABARZON (Region IV-A), MIMAROPA (Region IV-B), Bicol Region (Region V), Cordillera Administrative Region (CAR), Western Visayas (Region VI), Central Visayas (Region VII), Eastern Visayas (Region VIII), Zamboanga Peninsula (Region IX), Northern Mindanao (Region X), Davao Region (Region XI), Soccsksargen (Region XII), Caraga (Region XIII), Autonomous Region in Muslim Mindanao (ARMM)
––––––––––
Company/Owner: AJU Global Transport Corporation/King Coach Tours and Transport Corporation
Fleet/Bus Number: 840
Classification: Air-conditioned Tourist Chartered Bus
Coachbuilder: Kia Motors Corporation
Body Model: Kia Granbird SD-II Parkway
Engine Model: Hyundai D6AC (Q340)
Chassis Model: Kia KM949S (KN2GBJ722YK)
Transmission: 5-speed Manual Transmission
Suspension(s): Air Suspension
Seating Configuration: 2+1×2
Seating Capacity: 60 (49+11 jump-seats)
Franchise route: N/A
Route: various (Tourist Chartered)
Municipalities/cities passing: N/A
Type of Operation: Tourist Operation Non-Public Utility Bus (Special Trip/Tourist Class)
Area of Operation: Any point of Luzon: Ilocos Region (Region I), Cagayan Valley (Region II), Central Luzon (Region III), CALABARZON (Region IV-A), MIMAROPA (Region IV-B), Bicol Region (Region V), Cordillera Administrative Region (CAR)
Shot location: In-front of Barasoain Church, Malolos City, Bulacan
Date and time taken: September 24, 2015 (7:33H)
Notices:
* Please DON'T GRAB A PHOTO WITHOUT A PERMISSION. If you're going to GRAB IT, please give A CREDIT TO THE OWNER. Also, don't PRINT SCREEN my photos.
** If I have mistakes on the specifications, please comment in a good manner so that I can edit it immediately.
*** The specifications mentioned above are subjected for verification and may be changed without prior notice.
**** The vehicle's registration plate(s), conduction sticker(s), and/or persons (if applicable) were pixelated/blurred to prevent any conflict with the photographer, the bus company and/or to the car owner for their security and/or privacy purposes. So, don't use their plate number, conduction sticker, and vehicle tag as an evidence for any incident. And, I have taken this photo for bus fanatics, bus enthusiasts, and bus lovers purposes.
The Supermarine Spitfire is a British single-seat fighter aircraft that was used by the Royal Air Force and many other Allied countries during and after the Second World War. The Spitfire was built in many variants, using several wing configurations, and was produced in greater numbers than any other British aircraft. It was also the only British fighter to be in continuous production throughout the war. The Spitfire continues to be a popular aircraft, with approximately 55 Spitfires being airworthy, while many more are static exhibits in aviation museums all over the world.
The Spitfire was designed as a short-range, high-performance interceptor aircraft by R. J. Mitchell, chief designer at Supermarine Aviation Works (which operated as a subsidiary of Vickers-Armstrong from 1928). In accordance with its role as an interceptor, Mitchell designed the Spitfire's distinctive elliptical wing to have the thinnest possible cross-section; this thin wing enabled the Spitfire to have a higher top speed than several contemporary fighters, including the Hawker Hurricane. Mitchell continued to refine the design until his death from cancer in 1937, whereupon his colleague Joseph Smith took over as chief designer, overseeing the development of the Spitfire through its multitude of variants.
During the Battle of Britain (July–October 1940), the Spitfire was perceived by the public to be the RAF fighter, though the more numerous Hawker Hurricane shouldered a greater proportion of the burden against the Luftwaffe. However, because of its higher performance, Spitfire units had a lower attrition rate and a higher victory-to-loss ratio than those flying Hurricanes.
After the Battle of Britain, the Spitfire superseded the Hurricane to become the backbone of RAF Fighter Command, and saw action in the European, Mediterranean, Pacific and the South-East Asian theatres. Much loved by its pilots, the Spitfire served in several roles, including interceptor, photo-reconnaissance, fighter-bomber and trainer, and it continued to serve in these roles until the 1950s. The Seafire was a carrier-based adaptation of the Spitfire which served in the Fleet Air Arm from 1942 through to the mid-1950s. Although the original airframe was designed to be powered by a Rolls-Royce Merlin engine producing 1,030 hp (768 kW), it was strong enough and adaptable enough to use increasingly powerful Merlin and, in later marks, Rolls-Royce Griffon engines producing up to 2,340 hp (1,745 kW); as a consequence of this the Spitfire's performance and capabilities improved, sometimes dramatically, over the course of its life.
Mk V (Types 331, 349 & 352)
Spitfire LF.Mk VB, BL479, flown by Group Captain M.W.S Robinson, station commander of RAF Northolt, August 1943. This Spitfire has the wide bladed Rotol propeller, the internal armoured windscreen and "clipped" wings.
Late in 1940, the RAF predicted that the advent of the pressurised Junkers Ju 86P bomber series over Britain would be the start of a new sustained high altitude bombing offensive by the Luftwaffe, in which case development was put in hand for a pressurised version of the Spitfire, with a new version of the Merlin (the Mk VI). It would take some time to develop the new fighter and an emergency stop-gap measure was needed as soon as possible: this was the Mk V.
The basic Mk V was a Mk I with the Merlin 45 series engine. This engine delivered 1,440 hp (1,074 kW) at take-off, and incorporated a new single-speed single-stage supercharger design. Improvements to the carburettor also allowed the Spitfire to use zero gravity manoeuvres without any problems with fuel flow. Several Mk I and Mk II airframes were converted to Mk V standard by Supermarine and started equipping fighter units from early 1941. The majority of the Mk Vs were built at Castle Bromwich.
The VB became the main production version of the Mark Vs. Along with the new Merlin 45 series the B wing was fitted as standard. As production progressed changes were incorporated, some of which became standard on all later Spitfires. Production started with several Mk IBs which were converted to Mk VBs by Supermarine. Starting in early 1941 the round section exhaust stacks were changed to a "fishtail" type, marginally increasing exhaust thrust. Some late production VBs and VCs were fitted with six shorter exhaust stacks per side, similar to those of Spitfire IXs and Seafire IIIs; this was originally stipulated as applying specifically to VB(trop)s. After some initial problems with the original Mk I size oil coolers, a bigger oil cooler was fitted under the port wing; this could be recognised by a deeper housing with a circular entry. From mid-1941 alloy covered ailerons became a universal fitting.
Spitfire VC(trop), fitted with Vokes filters and "disc" wheels, of 417 Squadron RCAF in Tunisia in 1943.
A constant flow of modifications were made as production progressed. A "blown" cockpit hood, manufactured by Malcolm, was introduced in an effort to further increase the pilot's head-room and visibility. Many mid to late production VBs - and all VCs - used the modified, improved windscreen assembly with the integral bullet resistant centre panel and flat side screens introduced with the Mk III. Because the rear frame of this windscreen was taller than that of the earlier model the cockpit hoods were not interchangeable and could be distinguished by the wider rear framing on the hood used with the late-style windscreen.
Different propeller types were fitted, according to where the Spitfire V was built: Supermarine and Westland manufactured VBs and VCs used 10 ft 9 in (3.28 m) diameter, 3 bladed de Havilland constant speed units, with narrow metal blades, while Castle Bromwich manufactured VBs and VCs were fitted with a wide bladed Rotol constant speed propeller of either 10 ft 9 in (3.28 m) diameter, with metal blades, or (on late production Spitfires) 10 ft 3 in (3.12 m) diameter, with broader, "Jablo" (compressed wood) blades. The Rotol spinners were longer and more pointed than the de Havilland leading to a 3.5 in (8.9 cm) increase in overall length. The Rotol propellers allowed a modest speed increase over 20,000 ft (6,100 m) and an increase in the service ceiling. A large number of Spitfire VBs were fitted with "gun heater intensifier" systems on the exhaust stacks. These piped additional heated air into the gun bays. There was a short tubular intake on the front of the first stack and a narrow pipe led into the engine cowling from the rear exhaust.
The VB series were the first Spitfires able to carry a range of specially designed "slipper" drop tanks which were fitted underneath the wing centre-section. Small hooks were fitted, just forward of the inboard flaps: when the tank was released these hooks caught the trailing edge of the tank, swinging it clear of the fuselage.
With the advent of the superb Focke Wulf Fw 190 in August 1941 the Spitfire was for the first time truly outclassed, hastening the development of the "interim" Mk IX. In an effort to counter this threat, especially at lower altitudes, the VB was the first production version of the Spitfire to use "clipped" wingtips as an option, reducing the wingspan to 32 ft 2 in (9.8 m).The clipped wings increased the roll rate and airspeed at lower altitudes. Several different versions of the Merlin 45/50 family were used, including the Merlin 45M which had a smaller "cropped" supercharger impeller and boost increased to +18 lb. This engine produced 1,585 hp (1,182 kW) at 2,750 ft (838 m), increasing the L.F VB's maximum rate of climb to 4720 ft/min (21.6 m/s) at 2,000 ft (610 m).
VB Trop of 40 Squadron SAAF fitted with the "streamlined" version of the Aboukir filter, a broad-bladed, 10 ft 3 in (3.12 m) diameter Rotol propeller, and clipped wings.
The Mk VB(trop) (or type 352) could be identified by the large Vokes air filter fitted under the nose; the reduced speed of the air to the supercharger had a detrimental effect on the performance of the aircraft, reducing the top speed by 8 mph (13 km/h) and the climb rate by 600 ft/min (3.04 m/s), but the decreased performance was considered acceptable. This variant was also fitted with a larger oil tank and desert survival gear behind the pilot's seat. A new "desert" camouflage scheme was applied. Many VB(trop)s were modified by 103 MU (Maintenance Unit-RAF depots in which factory fresh aircraft were brought up to service standards before being delivered to squadrons) at Aboukir, Egypt by replacing the Vokes filter with locally manufactured "Aboukir" filters, which were lighter and more streamlined. Two designs of these filters can be identified in photos: one had a bulky, squared off filter housing while the other was more streamlined. These aircraft were usually fitted with the wide blade Rotol propeller and clipped wings.
Triumph Spitfire Mk I Roadster
The Triumph Spitfire is a small English two-seat sports car, introduced at the London Motor Show in 1962.[3] The vehicle was based on a design produced for Standard-Triumph in 1957 by Italian designer Giovanni Michelotti. The platform for the car was largely based upon the chassis, engine, and running gear of the Triumph Herald saloon, and was manufactured at the Standard-Triumph works at Canley, in Coventry. As was typical for cars of this era, the bodywork was fitted onto a separate structural chassis, but for the Spitfire, which was designed as an open top or convertible sports car from the outset, the ladder chassis was reinforced for additional rigidity by the use of structural components within the bodywork. The Spitfire was provided with a manual hood for weather protection, the design improving to a folding hood for later models. Factory-manufactured hard-tops were also available.
The Triumph Spitfire was originally devised by Standard-Triumph to compete in the small sports car market that had opened up with the introduction of the Austin-Healey Sprite. The Sprite had used the basic drive train of the Austin A30/35 in a light body to make up a budget sports car; Triumph's idea was to use the mechanicals from their small saloon, the Herald, to underpin the new project. Triumph had one advantage, however; where the Austin A30 range was of unitary construction, the Herald featured a separate chassis. It was Triumph's intention to cut that chassis down and clothe it in a sports body, saving the costs of developing a completely new chassis / body unit.
Italian designer Michelotti—who had already penned the Herald—was commissioned for the new project, and came up with a traditional, swooping body. Wind-up windows were provided (in contrast to the Sprite/Midget, which still featured sidescreens, also called curtains, at that time), as well as a single-piece front end which tilted forwards to offer unrivaled access to the engine. At the dawn of the 1960s, however, Standard-Triumph was in deep financial trouble, and unable to put the new car into production; it was not until the company was taken over by the Leyland organization funds became available and the car was launched. Leyland officials, taking stock of their new acquisition, found Michelotti's prototype hiding under a dust sheet in a corner of the factory and rapidly approved it for production.
Spitfire 4 or Mark I (1962-1964)
Overview:
Production1962–1964
45,753 made
Powertrain:
Engine1,147 cc (1.1 l) I4
Transmission4-speed manual with optional overdrive on top and third from 1963 onwards
Dimensions:
Curb weight1,568 lb (711 kg) (unladen U.K.-spec)
The production car changed little from the prototype, although the full-width rear bumper was dropped in favour of two part-bumpers curving round each corner, with overriders. Mechanicals were basically stock Herald. The engine was an 1,147 cc (1.1 l) 4-cylinder with a pushrod OHV cylinder head and 2 valves per cylinder, mildly tuned for the Spitfire, fed by twin SU carburettors. Also from the Herald came the rack and pinion steering and coil-and-wishbone front suspension up front, and at the rear a single transverse-leaf swing axle arrangement. This ended up being the most controversial part of the car: it was known to "tuck in" and cause violent over steer if pushed too hard, even in the staid Herald. In the sportier Spitfire (and later the 6-cylinder Triumph GT6 and Triumph Vitesse) it led to severe criticism. The body was bolted to a much-modified Herald chassis, the outer rails and the rear outriggers having been removed; little of the original Herald chassis design was left, and the Spitfire used structural outer sills to stiffen its body tub.
The Spitfire was an inexpensive small sports car and as such had very basic trim, including rubber mats and a large plastic steering wheel. These early cars were referred to both as "Triumph Spitfire Mark I" and "Spitfire 4", not to be confused with the later Spitfire Mark IV.
In UK specification the in-line four produced 63 bhp (47 kW) at 5750 rpm, and 67 lb·ft (91 N·m)of torque at 3500 rpm. This gave a top speed of 92 mph (148 km/h), and would achieve 0 to 60 mph (97 km/h) in 17.3 seconds. Average fuel consumption was 31mpg.
For 1964 an overdrive option was added to the 4-speed manual gearbox to give more relaxed cruising. Wire wheels and a hard top were also available.
Text regarding the Supermarine Spitfire aeroplane and Triumph Spitfire Roadster has been taken from excerpts of Wikipedia articles on each model.
The Supermarine Spitfire Mk VB aircraft and 1962 Triumph Spitfire Mk I road car have been modelled in Lego miniland-scale for Flickr LUGNuts' 79th Build Challenge, - 'LUGNuts goes Wingnuts, ' - featuring automotive vehicles named after, inspired by, or with some relationship to aircraft.
To set what extra information you want to see on the photo page, go to the More info page (by clicking on the camera name in the top right of the photo page) and check/uncheck the fields you want to see.
Company/Owner: JoyBus/Genesis Transport Services, Inc.
Fleet/Bus Number: 81863*
Classification: Air-conditioned First Class Provincial/Tourist Chartered Bus (with restroom)
Coachbuilder: Zhongtong Bus Holding Company, Ltd.
Body Model: Zhongtong LCK6128H Magnate
Engine Model: Yuchai YC6L330-30 (L47RA)
Chassis Model: Zhongtong LCK6**** (LDYCCS2C5H)
Transmission: 6-speed Manual Transmission
Suspension: Air Suspension
Seating Configuration: 2×1
Seating Capacity: 28
Franchise Route: Baguio City–Domestic via North Expressway EDSA
Route: Baguio City, Benguet–Pasay City via N208 (Aspiras–Palispis Highway/Marcos Highway/Agoo–Baguio) / N209 (Pugo–Rosario Road)) / E1 (TPLEX-Pozorrubio–NLEX-Balintawak)
Municipalities/cities passing: Tuba/Pugo/Rosario/Sison/Pozorrubio
Type of Operation: Provincial Operation Public Utility Bus (Premier Class/First Class; Tourist Class)
Area of Operation: Cordillera Administrative Region (CAR)
Shot location: NLEX-Bocaue, Bulacan
Date and time taken: May 16, 2018 (7:14H)
Notices:
* Please DON'T GRAB A PHOTO WITHOUT A PERMISSION. If you're going to GRAB IT, please give A CREDIT TO THE OWNER. Also, don't PRINT SCREEN my photos.
** If I have mistakes on the specifications, please comment in a good manner so that I can edit it immediately.
*** The specifications and routes (for provincial, inter-provincial, and city operation) mentioned above are subjected for verification and may be changed without prior notice.
**** The vehicle's registration plate(s), conduction sticker(s), and/or persons (if applicable) were pixelated/blurred to prevent any conflict with the photographer, the bus company and/or to the car owner for their security and/or privacy purposes. So, don't use their plate number, conduction sticker, and vehicle tag as an evidence for any incident. And, I have taken this photo for bus fanatics, bus enthusiasts, and bus lovers purposes.
Bus Operator: Solid North Transit
Bus No: 1615
Year released: 2010
Capacity: 45; 2x2 seating configuration
Body: Yutong Bus Ltd.
Model: 2010 Yutong ZK6107H Series
Engine: Yuchai
Fare: Airconditioned
Aircon System: Yutong overhead a/c
Transmission System: M/T
Shot Location: SM North EDSA
The Supermarine Spitfire is a British single-seat fighter aircraft that was used by the Royal Air Force and many other Allied countries during and after the Second World War. The Spitfire was built in many variants, using several wing configurations, and was produced in greater numbers than any other British aircraft. It was also the only British fighter to be in continuous production throughout the war. The Spitfire continues to be a popular aircraft, with approximately 55 Spitfires being airworthy, while many more are static exhibits in aviation museums all over the world.
The Spitfire was designed as a short-range, high-performance interceptor aircraft by R. J. Mitchell, chief designer at Supermarine Aviation Works (which operated as a subsidiary of Vickers-Armstrong from 1928). In accordance with its role as an interceptor, Mitchell designed the Spitfire's distinctive elliptical wing to have the thinnest possible cross-section; this thin wing enabled the Spitfire to have a higher top speed than several contemporary fighters, including the Hawker Hurricane. Mitchell continued to refine the design until his death from cancer in 1937, whereupon his colleague Joseph Smith took over as chief designer, overseeing the development of the Spitfire through its multitude of variants.
During the Battle of Britain (July–October 1940), the Spitfire was perceived by the public to be the RAF fighter, though the more numerous Hawker Hurricane shouldered a greater proportion of the burden against the Luftwaffe. However, because of its higher performance, Spitfire units had a lower attrition rate and a higher victory-to-loss ratio than those flying Hurricanes.
After the Battle of Britain, the Spitfire superseded the Hurricane to become the backbone of RAF Fighter Command, and saw action in the European, Mediterranean, Pacific and the South-East Asian theatres. Much loved by its pilots, the Spitfire served in several roles, including interceptor, photo-reconnaissance, fighter-bomber and trainer, and it continued to serve in these roles until the 1950s. The Seafire was a carrier-based adaptation of the Spitfire which served in the Fleet Air Arm from 1942 through to the mid-1950s. Although the original airframe was designed to be powered by a Rolls-Royce Merlin engine producing 1,030 hp (768 kW), it was strong enough and adaptable enough to use increasingly powerful Merlin and, in later marks, Rolls-Royce Griffon engines producing up to 2,340 hp (1,745 kW); as a consequence of this the Spitfire's performance and capabilities improved, sometimes dramatically, over the course of its life.
Mk V (Types 331, 349 & 352)
Spitfire LF.Mk VB, BL479, flown by Group Captain M.W.S Robinson, station commander of RAF Northolt, August 1943. This Spitfire has the wide bladed Rotol propeller, the internal armoured windscreen and "clipped" wings.
Late in 1940, the RAF predicted that the advent of the pressurised Junkers Ju 86P bomber series over Britain would be the start of a new sustained high altitude bombing offensive by the Luftwaffe, in which case development was put in hand for a pressurised version of the Spitfire, with a new version of the Merlin (the Mk VI). It would take some time to develop the new fighter and an emergency stop-gap measure was needed as soon as possible: this was the Mk V.
The basic Mk V was a Mk I with the Merlin 45 series engine. This engine delivered 1,440 hp (1,074 kW) at take-off, and incorporated a new single-speed single-stage supercharger design. Improvements to the carburettor also allowed the Spitfire to use zero gravity manoeuvres without any problems with fuel flow. Several Mk I and Mk II airframes were converted to Mk V standard by Supermarine and started equipping fighter units from early 1941. The majority of the Mk Vs were built at Castle Bromwich.
The VB became the main production version of the Mark Vs. Along with the new Merlin 45 series the B wing was fitted as standard. As production progressed changes were incorporated, some of which became standard on all later Spitfires. Production started with several Mk IBs which were converted to Mk VBs by Supermarine. Starting in early 1941 the round section exhaust stacks were changed to a "fishtail" type, marginally increasing exhaust thrust. Some late production VBs and VCs were fitted with six shorter exhaust stacks per side, similar to those of Spitfire IXs and Seafire IIIs; this was originally stipulated as applying specifically to VB(trop)s. After some initial problems with the original Mk I size oil coolers, a bigger oil cooler was fitted under the port wing; this could be recognised by a deeper housing with a circular entry. From mid-1941 alloy covered ailerons became a universal fitting.
Spitfire VC(trop), fitted with Vokes filters and "disc" wheels, of 417 Squadron RCAF in Tunisia in 1943.
A constant flow of modifications were made as production progressed. A "blown" cockpit hood, manufactured by Malcolm, was introduced in an effort to further increase the pilot's head-room and visibility. Many mid to late production VBs - and all VCs - used the modified, improved windscreen assembly with the integral bullet resistant centre panel and flat side screens introduced with the Mk III. Because the rear frame of this windscreen was taller than that of the earlier model the cockpit hoods were not interchangeable and could be distinguished by the wider rear framing on the hood used with the late-style windscreen.
Different propeller types were fitted, according to where the Spitfire V was built: Supermarine and Westland manufactured VBs and VCs used 10 ft 9 in (3.28 m) diameter, 3 bladed de Havilland constant speed units, with narrow metal blades, while Castle Bromwich manufactured VBs and VCs were fitted with a wide bladed Rotol constant speed propeller of either 10 ft 9 in (3.28 m) diameter, with metal blades, or (on late production Spitfires) 10 ft 3 in (3.12 m) diameter, with broader, "Jablo" (compressed wood) blades. The Rotol spinners were longer and more pointed than the de Havilland leading to a 3.5 in (8.9 cm) increase in overall length. The Rotol propellers allowed a modest speed increase over 20,000 ft (6,100 m) and an increase in the service ceiling. A large number of Spitfire VBs were fitted with "gun heater intensifier" systems on the exhaust stacks. These piped additional heated air into the gun bays. There was a short tubular intake on the front of the first stack and a narrow pipe led into the engine cowling from the rear exhaust.
The VB series were the first Spitfires able to carry a range of specially designed "slipper" drop tanks which were fitted underneath the wing centre-section. Small hooks were fitted, just forward of the inboard flaps: when the tank was released these hooks caught the trailing edge of the tank, swinging it clear of the fuselage.
With the advent of the superb Focke Wulf Fw 190 in August 1941 the Spitfire was for the first time truly outclassed, hastening the development of the "interim" Mk IX. In an effort to counter this threat, especially at lower altitudes, the VB was the first production version of the Spitfire to use "clipped" wingtips as an option, reducing the wingspan to 32 ft 2 in (9.8 m).The clipped wings increased the roll rate and airspeed at lower altitudes. Several different versions of the Merlin 45/50 family were used, including the Merlin 45M which had a smaller "cropped" supercharger impeller and boost increased to +18 lb. This engine produced 1,585 hp (1,182 kW) at 2,750 ft (838 m), increasing the L.F VB's maximum rate of climb to 4720 ft/min (21.6 m/s) at 2,000 ft (610 m).
VB Trop of 40 Squadron SAAF fitted with the "streamlined" version of the Aboukir filter, a broad-bladed, 10 ft 3 in (3.12 m) diameter Rotol propeller, and clipped wings.
The Mk VB(trop) (or type 352) could be identified by the large Vokes air filter fitted under the nose; the reduced speed of the air to the supercharger had a detrimental effect on the performance of the aircraft, reducing the top speed by 8 mph (13 km/h) and the climb rate by 600 ft/min (3.04 m/s), but the decreased performance was considered acceptable. This variant was also fitted with a larger oil tank and desert survival gear behind the pilot's seat. A new "desert" camouflage scheme was applied. Many VB(trop)s were modified by 103 MU (Maintenance Unit-RAF depots in which factory fresh aircraft were brought up to service standards before being delivered to squadrons) at Aboukir, Egypt by replacing the Vokes filter with locally manufactured "Aboukir" filters, which were lighter and more streamlined. Two designs of these filters can be identified in photos: one had a bulky, squared off filter housing while the other was more streamlined. These aircraft were usually fitted with the wide blade Rotol propeller and clipped wings.
Triumph Spitfire Mk I Roadster
The Triumph Spitfire is a small English two-seat sports car, introduced at the London Motor Show in 1962.[3] The vehicle was based on a design produced for Standard-Triumph in 1957 by Italian designer Giovanni Michelotti. The platform for the car was largely based upon the chassis, engine, and running gear of the Triumph Herald saloon, and was manufactured at the Standard-Triumph works at Canley, in Coventry. As was typical for cars of this era, the bodywork was fitted onto a separate structural chassis, but for the Spitfire, which was designed as an open top or convertible sports car from the outset, the ladder chassis was reinforced for additional rigidity by the use of structural components within the bodywork. The Spitfire was provided with a manual hood for weather protection, the design improving to a folding hood for later models. Factory-manufactured hard-tops were also available.
The Triumph Spitfire was originally devised by Standard-Triumph to compete in the small sports car market that had opened up with the introduction of the Austin-Healey Sprite. The Sprite had used the basic drive train of the Austin A30/35 in a light body to make up a budget sports car; Triumph's idea was to use the mechanicals from their small saloon, the Herald, to underpin the new project. Triumph had one advantage, however; where the Austin A30 range was of unitary construction, the Herald featured a separate chassis. It was Triumph's intention to cut that chassis down and clothe it in a sports body, saving the costs of developing a completely new chassis / body unit.
Italian designer Michelotti—who had already penned the Herald—was commissioned for the new project, and came up with a traditional, swooping body. Wind-up windows were provided (in contrast to the Sprite/Midget, which still featured sidescreens, also called curtains, at that time), as well as a single-piece front end which tilted forwards to offer unrivaled access to the engine. At the dawn of the 1960s, however, Standard-Triumph was in deep financial trouble, and unable to put the new car into production; it was not until the company was taken over by the Leyland organization funds became available and the car was launched. Leyland officials, taking stock of their new acquisition, found Michelotti's prototype hiding under a dust sheet in a corner of the factory and rapidly approved it for production.
Spitfire 4 or Mark I (1962-1964)
Overview:
Production1962–1964
45,753 made
Powertrain:
Engine1,147 cc (1.1 l) I4
Transmission4-speed manual with optional overdrive on top and third from 1963 onwards
Dimensions:
Curb weight1,568 lb (711 kg) (unladen U.K.-spec)
The production car changed little from the prototype, although the full-width rear bumper was dropped in favour of two part-bumpers curving round each corner, with overriders. Mechanicals were basically stock Herald. The engine was an 1,147 cc (1.1 l) 4-cylinder with a pushrod OHV cylinder head and 2 valves per cylinder, mildly tuned for the Spitfire, fed by twin SU carburettors. Also from the Herald came the rack and pinion steering and coil-and-wishbone front suspension up front, and at the rear a single transverse-leaf swing axle arrangement. This ended up being the most controversial part of the car: it was known to "tuck in" and cause violent over steer if pushed too hard, even in the staid Herald. In the sportier Spitfire (and later the 6-cylinder Triumph GT6 and Triumph Vitesse) it led to severe criticism. The body was bolted to a much-modified Herald chassis, the outer rails and the rear outriggers having been removed; little of the original Herald chassis design was left, and the Spitfire used structural outer sills to stiffen its body tub.
The Spitfire was an inexpensive small sports car and as such had very basic trim, including rubber mats and a large plastic steering wheel. These early cars were referred to both as "Triumph Spitfire Mark I" and "Spitfire 4", not to be confused with the later Spitfire Mark IV.
In UK specification the in-line four produced 63 bhp (47 kW) at 5750 rpm, and 67 lb·ft (91 N·m)of torque at 3500 rpm. This gave a top speed of 92 mph (148 km/h), and would achieve 0 to 60 mph (97 km/h) in 17.3 seconds. Average fuel consumption was 31mpg.
For 1964 an overdrive option was added to the 4-speed manual gearbox to give more relaxed cruising. Wire wheels and a hard top were also available.
Text regarding the Supermarine Spitfire aeroplane and Triumph Spitfire Roadster has been taken from excerpts of Wikipedia articles on each model.
The Supermarine Spitfire Mk VB aircraft and 1962 Triumph Spitfire Mk I road car have been modelled in Lego miniland-scale for Flickr LUGNuts' 79th Build Challenge, - 'LUGNuts goes Wingnuts, ' - featuring automotive vehicles named after, inspired by, or with some relationship to aircraft.
PEÑAFRANCIA Tours and Travel Transport, Inc
Bus Number: 8
Coachbuilder: Almazora Motors, Corporation
Chassis: Mercedes-Benz O500M 1725
Model: AMC Tourist Star RE Deluxe
Engine: Mercedes-Benz OM906LA
Airconditioning Unit: Overhead Unit
Suspension: Air-Suspension
Seating Configuration: 2x1
Seating Capacity: 22 Passengers
Shot Location:
Demon Configuration: 2Ra+d8 / 2Rm / 1G / 2W
===========================================================
Built for Mobile Frame Zero - a tabletop wargame.
Mobile Frame Hangar (MFZ Community Forums).
===========================================================
The Supermarine Spitfire is a British single-seat fighter aircraft that was used by the Royal Air Force and many other Allied countries during and after the Second World War. The Spitfire was built in many variants, using several wing configurations, and was produced in greater numbers than any other British aircraft. It was also the only British fighter to be in continuous production throughout the war. The Spitfire continues to be a popular aircraft, with approximately 55 Spitfires being airworthy, while many more are static exhibits in aviation museums all over the world.
The Spitfire was designed as a short-range, high-performance interceptor aircraft by R. J. Mitchell, chief designer at Supermarine Aviation Works (which operated as a subsidiary of Vickers-Armstrong from 1928). In accordance with its role as an interceptor, Mitchell designed the Spitfire's distinctive elliptical wing to have the thinnest possible cross-section; this thin wing enabled the Spitfire to have a higher top speed than several contemporary fighters, including the Hawker Hurricane. Mitchell continued to refine the design until his death from cancer in 1937, whereupon his colleague Joseph Smith took over as chief designer, overseeing the development of the Spitfire through its multitude of variants.
During the Battle of Britain (July–October 1940), the Spitfire was perceived by the public to be the RAF fighter, though the more numerous Hawker Hurricane shouldered a greater proportion of the burden against the Luftwaffe. However, because of its higher performance, Spitfire units had a lower attrition rate and a higher victory-to-loss ratio than those flying Hurricanes.
After the Battle of Britain, the Spitfire superseded the Hurricane to become the backbone of RAF Fighter Command, and saw action in the European, Mediterranean, Pacific and the South-East Asian theatres. Much loved by its pilots, the Spitfire served in several roles, including interceptor, photo-reconnaissance, fighter-bomber and trainer, and it continued to serve in these roles until the 1950s. The Seafire was a carrier-based adaptation of the Spitfire which served in the Fleet Air Arm from 1942 through to the mid-1950s. Although the original airframe was designed to be powered by a Rolls-Royce Merlin engine producing 1,030 hp (768 kW), it was strong enough and adaptable enough to use increasingly powerful Merlin and, in later marks, Rolls-Royce Griffon engines producing up to 2,340 hp (1,745 kW); as a consequence of this the Spitfire's performance and capabilities improved, sometimes dramatically, over the course of its life.
Mk V (Types 331, 349 & 352)
Spitfire LF.Mk VB, BL479, flown by Group Captain M.W.S Robinson, station commander of RAF Northolt, August 1943. This Spitfire has the wide bladed Rotol propeller, the internal armoured windscreen and "clipped" wings.
Late in 1940, the RAF predicted that the advent of the pressurised Junkers Ju 86P bomber series over Britain would be the start of a new sustained high altitude bombing offensive by the Luftwaffe, in which case development was put in hand for a pressurised version of the Spitfire, with a new version of the Merlin (the Mk VI). It would take some time to develop the new fighter and an emergency stop-gap measure was needed as soon as possible: this was the Mk V.
The basic Mk V was a Mk I with the Merlin 45 series engine. This engine delivered 1,440 hp (1,074 kW) at take-off, and incorporated a new single-speed single-stage supercharger design. Improvements to the carburettor also allowed the Spitfire to use zero gravity manoeuvres without any problems with fuel flow. Several Mk I and Mk II airframes were converted to Mk V standard by Supermarine and started equipping fighter units from early 1941. The majority of the Mk Vs were built at Castle Bromwich.
The VB became the main production version of the Mark Vs. Along with the new Merlin 45 series the B wing was fitted as standard. As production progressed changes were incorporated, some of which became standard on all later Spitfires. Production started with several Mk IBs which were converted to Mk VBs by Supermarine. Starting in early 1941 the round section exhaust stacks were changed to a "fishtail" type, marginally increasing exhaust thrust. Some late production VBs and VCs were fitted with six shorter exhaust stacks per side, similar to those of Spitfire IXs and Seafire IIIs; this was originally stipulated as applying specifically to VB(trop)s. After some initial problems with the original Mk I size oil coolers, a bigger oil cooler was fitted under the port wing; this could be recognised by a deeper housing with a circular entry. From mid-1941 alloy covered ailerons became a universal fitting.
Spitfire VC(trop), fitted with Vokes filters and "disc" wheels, of 417 Squadron RCAF in Tunisia in 1943.
A constant flow of modifications were made as production progressed. A "blown" cockpit hood, manufactured by Malcolm, was introduced in an effort to further increase the pilot's head-room and visibility. Many mid to late production VBs - and all VCs - used the modified, improved windscreen assembly with the integral bullet resistant centre panel and flat side screens introduced with the Mk III. Because the rear frame of this windscreen was taller than that of the earlier model the cockpit hoods were not interchangeable and could be distinguished by the wider rear framing on the hood used with the late-style windscreen.
Different propeller types were fitted, according to where the Spitfire V was built: Supermarine and Westland manufactured VBs and VCs used 10 ft 9 in (3.28 m) diameter, 3 bladed de Havilland constant speed units, with narrow metal blades, while Castle Bromwich manufactured VBs and VCs were fitted with a wide bladed Rotol constant speed propeller of either 10 ft 9 in (3.28 m) diameter, with metal blades, or (on late production Spitfires) 10 ft 3 in (3.12 m) diameter, with broader, "Jablo" (compressed wood) blades. The Rotol spinners were longer and more pointed than the de Havilland leading to a 3.5 in (8.9 cm) increase in overall length. The Rotol propellers allowed a modest speed increase over 20,000 ft (6,100 m) and an increase in the service ceiling. A large number of Spitfire VBs were fitted with "gun heater intensifier" systems on the exhaust stacks. These piped additional heated air into the gun bays. There was a short tubular intake on the front of the first stack and a narrow pipe led into the engine cowling from the rear exhaust.
The VB series were the first Spitfires able to carry a range of specially designed "slipper" drop tanks which were fitted underneath the wing centre-section. Small hooks were fitted, just forward of the inboard flaps: when the tank was released these hooks caught the trailing edge of the tank, swinging it clear of the fuselage.
With the advent of the superb Focke Wulf Fw 190 in August 1941 the Spitfire was for the first time truly outclassed, hastening the development of the "interim" Mk IX. In an effort to counter this threat, especially at lower altitudes, the VB was the first production version of the Spitfire to use "clipped" wingtips as an option, reducing the wingspan to 32 ft 2 in (9.8 m).The clipped wings increased the roll rate and airspeed at lower altitudes. Several different versions of the Merlin 45/50 family were used, including the Merlin 45M which had a smaller "cropped" supercharger impeller and boost increased to +18 lb. This engine produced 1,585 hp (1,182 kW) at 2,750 ft (838 m), increasing the L.F VB's maximum rate of climb to 4720 ft/min (21.6 m/s) at 2,000 ft (610 m).
VB Trop of 40 Squadron SAAF fitted with the "streamlined" version of the Aboukir filter, a broad-bladed, 10 ft 3 in (3.12 m) diameter Rotol propeller, and clipped wings.
The Mk VB(trop) (or type 352) could be identified by the large Vokes air filter fitted under the nose; the reduced speed of the air to the supercharger had a detrimental effect on the performance of the aircraft, reducing the top speed by 8 mph (13 km/h) and the climb rate by 600 ft/min (3.04 m/s), but the decreased performance was considered acceptable. This variant was also fitted with a larger oil tank and desert survival gear behind the pilot's seat. A new "desert" camouflage scheme was applied. Many VB(trop)s were modified by 103 MU (Maintenance Unit-RAF depots in which factory fresh aircraft were brought up to service standards before being delivered to squadrons) at Aboukir, Egypt by replacing the Vokes filter with locally manufactured "Aboukir" filters, which were lighter and more streamlined. Two designs of these filters can be identified in photos: one had a bulky, squared off filter housing while the other was more streamlined. These aircraft were usually fitted with the wide blade Rotol propeller and clipped wings.
Triumph Spitfire Mk I Roadster
The Triumph Spitfire is a small English two-seat sports car, introduced at the London Motor Show in 1962.[3] The vehicle was based on a design produced for Standard-Triumph in 1957 by Italian designer Giovanni Michelotti. The platform for the car was largely based upon the chassis, engine, and running gear of the Triumph Herald saloon, and was manufactured at the Standard-Triumph works at Canley, in Coventry. As was typical for cars of this era, the bodywork was fitted onto a separate structural chassis, but for the Spitfire, which was designed as an open top or convertible sports car from the outset, the ladder chassis was reinforced for additional rigidity by the use of structural components within the bodywork. The Spitfire was provided with a manual hood for weather protection, the design improving to a folding hood for later models. Factory-manufactured hard-tops were also available.
The Triumph Spitfire was originally devised by Standard-Triumph to compete in the small sports car market that had opened up with the introduction of the Austin-Healey Sprite. The Sprite had used the basic drive train of the Austin A30/35 in a light body to make up a budget sports car; Triumph's idea was to use the mechanicals from their small saloon, the Herald, to underpin the new project. Triumph had one advantage, however; where the Austin A30 range was of unitary construction, the Herald featured a separate chassis. It was Triumph's intention to cut that chassis down and clothe it in a sports body, saving the costs of developing a completely new chassis / body unit.
Italian designer Michelotti—who had already penned the Herald—was commissioned for the new project, and came up with a traditional, swooping body. Wind-up windows were provided (in contrast to the Sprite/Midget, which still featured sidescreens, also called curtains, at that time), as well as a single-piece front end which tilted forwards to offer unrivaled access to the engine. At the dawn of the 1960s, however, Standard-Triumph was in deep financial trouble, and unable to put the new car into production; it was not until the company was taken over by the Leyland organization funds became available and the car was launched. Leyland officials, taking stock of their new acquisition, found Michelotti's prototype hiding under a dust sheet in a corner of the factory and rapidly approved it for production.
Spitfire 4 or Mark I (1962-1964)
Overview:
Production1962–1964
45,753 made
Powertrain:
Engine1,147 cc (1.1 l) I4
Transmission4-speed manual with optional overdrive on top and third from 1963 onwards
Dimensions:
Curb weight1,568 lb (711 kg) (unladen U.K.-spec)
The production car changed little from the prototype, although the full-width rear bumper was dropped in favour of two part-bumpers curving round each corner, with overriders. Mechanicals were basically stock Herald. The engine was an 1,147 cc (1.1 l) 4-cylinder with a pushrod OHV cylinder head and 2 valves per cylinder, mildly tuned for the Spitfire, fed by twin SU carburettors. Also from the Herald came the rack and pinion steering and coil-and-wishbone front suspension up front, and at the rear a single transverse-leaf swing axle arrangement. This ended up being the most controversial part of the car: it was known to "tuck in" and cause violent over steer if pushed too hard, even in the staid Herald. In the sportier Spitfire (and later the 6-cylinder Triumph GT6 and Triumph Vitesse) it led to severe criticism. The body was bolted to a much-modified Herald chassis, the outer rails and the rear outriggers having been removed; little of the original Herald chassis design was left, and the Spitfire used structural outer sills to stiffen its body tub.
The Spitfire was an inexpensive small sports car and as such had very basic trim, including rubber mats and a large plastic steering wheel. These early cars were referred to both as "Triumph Spitfire Mark I" and "Spitfire 4", not to be confused with the later Spitfire Mark IV.
In UK specification the in-line four produced 63 bhp (47 kW) at 5750 rpm, and 67 lb·ft (91 N·m)of torque at 3500 rpm. This gave a top speed of 92 mph (148 km/h), and would achieve 0 to 60 mph (97 km/h) in 17.3 seconds. Average fuel consumption was 31mpg.
For 1964 an overdrive option was added to the 4-speed manual gearbox to give more relaxed cruising. Wire wheels and a hard top were also available.
Text regarding the Supermarine Spitfire aeroplane and Triumph Spitfire Roadster has been taken from excerpts of Wikipedia articles on each model.
The Supermarine Spitfire Mk VB aircraft and 1962 Triumph Spitfire Mk I road car have been modelled in Lego miniland-scale for Flickr LUGNuts' 79th Build Challenge, - 'LUGNuts goes Wingnuts, ' - featuring automotive vehicles named after, inspired by, or with some relationship to aircraft.
Victory Liner Inc.
Bus Number: 133
Classification: Airconditioned Provincial Operation Bus
Model: Hyundai Super Aero City
Manufacturer: Hyundai Motor Company
Chassis: Hyundai KMJTC18BPAC
Engine: Hyundai D6AB-D
Suspension: Leaf Spring Suspension
Seating Configuration: 3x2
Seating Capacity: 56 Passengers
Shot Location: Victory Liner Caloocan Terminal
Jets Flammable Tanker
Truck Manufacturer: MAN Truck & Bus AG
Model: TGS-WW
Chassis: 33.400
Engine: MAN D2066LF49
Suspension: Front: Leaf, Rear: Air
Axle Configuration: 6x4
Shot Location: A.boni, Balintawak
LNER Class A1 Peppercorn 60163 Tornado
Tornado, 14 December 2008
Power type
Steam
Designer
Arthur Peppercorn (original designer)
Builder
A1 Steam Locomotive Trust
Build date
1994–2008
Configuration
4-6-2
Leading wheel
diameter
3 ft 2 in (0.97 m)
Driver diameter
6 ft 8 in (2.03 m)
Trailing wheel
diameter
3 ft 8 in (1.12 m)
Length
72 ft 11.75 in (22.24 m)
Width
9 ft 2.875 in (2.82 m)
Height
13 ft (3.96 m)
Axle load
22.1 long tons (22.5 t)
Weight on drivers
66.55 long tons (67.62 t)
Locomotive weight
105.2 long tons (106.9 t)[1]
Tender weight
60.9 long tons (61.9 t)
Locomotive & tender
combined weight
166.1 long tons (168.8 t)
Fuel type
Coal
Fuel capacity
7.5 long tons (7.6 t))
Water capacity
6,000 imp gal (27,000 L))
Boiler
Diagram 118
6 ft 5 in (1.96 m) diameter
29 ft 2 in (8.89 m) length
Boiler pressure
250 psi (1,700 kPa)
Firegrate area
50.0 sq ft (4.65 m2)
Heating surface:
Tubes
1,211.6 sq ft (112.56 m2)
Heating surface:
Flues
1,004.5 sq ft (93.32 m2)
Heating surface:
Firebox
245.3 sq ft (22.79 m2)
Heating surface:
Total
2,461.4 sq ft (228.67 m2)
Superheater area
697.7 sq ft (64.82 m2)
Cylinder size
19 in × 26 in (480 mm × 660 mm)
Top speed
100 mph (160 km/h) design[2]
75 mph (121 km/h) certified
Tractive effort
2,700 metric horsepower (2,000 kW)
Number
60163 (display)
98863 (TOPS)
Official name
Tornado
Axle load class
Route availability 9
First run
29 July 2008
Disposition
Operational. Approved for 75 mph (121 km/h) running on the Network Rail main line.
60163 Tornado is a main-line steam locomotive built in Darlington, England. Completed in 2008, Tornado was the first such locomotive built in the United Kingdom since Evening Star, the last steam locomotive built by British Railways, in 1960. Designed to meet modern safety and certification standards, Tornado runs on the UK rail network and on mainline-connected heritage railways. The locomotive is named after the Panavia Tornado military jet.
Dominion Bus Lines
Bus Number: 80102
Manufacturer: Suzhou King Long United Automotive Industry Company, Ltd. (Higer Bus)
Body: Higer KLQ6125B1 - H92B
Suspension: Leaf-Speing Suspension
Engine: YuChai YC6L330-30
Chassis: Higer KLQ6120E3 (LKLR1KSL5BB)
Seat Configuration: 2x2
Capacity: 45
Shot Location: Balintawak
Oil Tanker Truck
Truck Manufacturer: MAN Truck & Bus AG
Model: TGA
Chassis: 33.360
Engine:
Suspension:
Axle Configuration: 6x4
Shot Location: A.boni
My new North American diesel engine in the Canadian Nation Railway scheme is the first Lego loco I have built since my childhood days and was strongly inspired by the EMD-GP 7, 9 and 20 diesel engines and other similar types that came in full high hood configuration, but I went on to building the model rather freely, leaving out things I didn’t want and not sticking to any particular real model.
Being 9+ studs wide, it’s quite a beast and fits very well to the “large city minifigure scale” preferred by ER0L and me. It drives on two 9V train motors from the 90s. The lighting is realized with materials from that time as well, energized by a separate battery box in the shorter section of the hood and thus illuminating the two fronts and cabin of the engine independently from the transformer. That way, the light can be on even when the model stands still.
I went for moving pilots, even though they don’t exist on such models in reality. This was mostly due to the prolonged bionicle trucks I wanted to use here, which would otherwise have made the stairs stand out too far from the trucks in curves and switches.
I have nearly finished building the first of several tank cars for it, so consider these pics an “opener” for more train equipment to come from me.
Goodmorning Universe
Bataan Transit Co., Inc
Bus Number: 712
Bus Manufacturer: Hyundai Motor Company (Korea)
Model: Hyundai Universe Xpress Noble
Chassis: Hyundai KMJKL18CP8C
Engine: Hyundai D6AC-Q
Suspension: Air Suspension
Seating Configuration: 2x2
Capacity: 45
Shot Location: Bataan Transir Doroteo Jose Terminal Avenida
Specifications
Engine
• VR-series twin-turbocharged 3.8-liter V6.
• 480 hp @ 6,800 rpm. 430 lb-ft torque @ 3,200–5,200 rpm.
• Dual overhead camshafts with variable intake-valve timing.
• Cast aluminum cylinder block with high-endurance/low-friction plasma-sprayed bores.
• IHI twin turbochargers, one per cylinder bank.
• Pressurized lubrication system with thermostatically controlled cooling.
Drivetrain
• ATTESA ET-S All-Wheel Drive (AWD) with independent rear-mounted transaxle integrating transmission, differential and AWD transfer case.
• Rigid, lightweight carbon-composite driveshaft between engine and transaxle.
• Electronic traction control plus 1.5-way mechanically locking rear differential.
• Vehicle Dynamics Control (VDC-R) with three driver-selectable settings: Normal (for daily driving, controls brakes and engine output), R-Mode (for ultimate performance, utilizes AWD torque distribution for additional vehicle stability) and Off (driver does not want the help of the system).
• Hill Start Assist prevents rollback when starting on an incline.
DisclaimerVDC-R cannot prevent accidents due to abrupt steering, carelessness, or dangerous driving techniques. Always drive safely.
Transmission
• 6-speed Dual Clutch Transmission with three driver-selectable modes: Normal (for maximum smoothness and efficiency), Snow (for gentler starting and shifting on slippery surfaces), and R mode (for maximum performance with fastest shifts).
• Fully automatic shifting or full sequential manual control via gearshift or steering wheel-mounted paddle shifters.
• Dual clutch design changes gears in less than 0.5 second (0.2 second in R mode).
• Downshift Rev Matching (DRM).
• Predictive pre-shift control (in R mode) based on throttle position, vehicle speed, braking and other information.
Wheels and Tires
• 20 x 9.5" (front) and 20 x 10.5" (rear) super-lightweight forged-aluminum wheels with Gunmetal Gray finish.
• Exclusively developed nitrogen-filled Bridgestone® RE070A high-capacity run-flat summer tires, 255/40R20 front and 285/35R20 rear.
• Tire Pressure Monitoring System (TPMS).
• Optional exclusively developed nitrogen-filled Dunlop® run-flat all-season tires, 255/40R20 front and 285/35R20 rear (includes Bright Silver wheels).
Brakes
• Brembo® 4-wheel disc brakes with 4-wheel Antilock Braking System (ABS), Brake Assist, Electronic Brakeforce Distribution and Preview Braking.
• Two-piece floating-rotor 15-inch front and rear discs with diamond-pattern internal ventilation.
• 6-piston front/4-piston rear monoblock calipers.
Steering
• Rack-and-pinion steering with vehicle-speed-sensitive power assist.
• 2.6 steering-wheel turns lock-to-lock.
Suspension
• 4-wheel independent suspension with Bilstein® DampTronic system with three driver-selectable modes: Normal/Sport (for automatic electronic control of damping), Comfort (for maximum ride comfort), and R mode (engages maximum damping rate for high-performance cornering).
• Electronically controlled variable-rate shock absorbers. High-accuracy progressive-rate coil springs.
• Front double-wishbone/rear multi-link configuration with aluminum members and rigid aluminum subframes.
• Hollow front and rear stabilizer bars.
Body/Chassis
• Exclusive Premium Midship platform with jig-welded hybrid unibody.
• Aluminum hood, trunk and door skins. Die-cast aluminum door structures.
• Carbon-reinforced front crossmember/radiator support.
Back to Top
Standard Features
Exterior
• Wide-beam headlights with High Intensity Discharge (HID) low beams.
• LED taillights and brake lights.
• Dual heated power mirrors.
• Flush-mounted aluminum door handles.
• Body-color rear spoiler with integrated center high-mounted stop light.
• UV-reducing tinted glass.
Audio/Navigation/Performance Monitor
• Digital Bose® audio system with AM/FM/in-dash 6-CD changer and 11 speakers including dual subwoofers.
• HDD Music Box system, including hard drive with 9.4 GB for audio storage.
• MP3, WMA and DVD audio capable. In-dash Compact Flash card reader.
• HDD-based GPS navigation with touch screen.
• Driver-configurable performance monitor, developed with Sony® Polyphony, with graphical readouts of vehicle data and driving data displayed on a total of 11 screens.
• 7-inch WVGA high-resolution color-LCD display for audio, navigation and performance monitor.
Interior
• Automatic Temperature Control (ATC).
• Electronic analog instrument cluster with multi-function trip computer and digital gear indicator.
• Power front windows with one-touch auto-up/down feature.
• Intelligent Key system with pushbutton start. Power door locks.
• Cruise control.
• Tilt/telescoping steering column.
• Bluetooth® Hands-free phone system with voice recognition.
Seating/Appointments
• Leather upholstered front seats with perforated Alcantara inserts.
• 8-way power front seats with entry/exit switch for rear-seat passengers.
• Driver-shaped bucket seat.
• Dual individual rear seats.
• Heated front seats.
• Leather-wrapped steering wheel and shift knob.
• Drilled aluminum pedals.
Safety/Security
• Nissan Advanced Air Bag System (AABS) with dual-stage supplemental front air bags, seat belt sensors and occupant-classification sensor.
• Driver and front-passenger side-impact supplemental air bags and roof-mounted curtain supplemental air bags.
• Front seat belts with pretensioners and load limiters.
• Nissan Vehicle Immobilizer System.
• Vehicle Security System.
Shell Oil Company
Truck Manufacturer: Volvo Philippines
Model: FM
Chassis
Engine:
Suspension:
Axle Configuration: 6x2 rearlift
Shot Location: Balintawak
Five Star Bus Company.
Bus Number: 88012
Model: Yutong ZK6119HA
Coachbuilder: Zhengzhou Yutong Bus Company, Ltd. (Yutong Bus)
Engine: Cummins C300-20
Classification: Airconditioned Provincial Operation Bus
Chassis: Yutong Zk6119CRA
Model: Yutong ZK6119HA
Engine: Cummins C300-20
Airconditioning Unit: Overhead Unit
Suspension: Air-Suspension
Seating Configuration: 2x2
Seating Capacity: 49 Passengers
Shot Location: Cubao
OMC
Truck Manufacturer: MAN Truck & Bus AG
Model: MAN TGS
Chassis 26.360
Engine:
Suspension:
Axle Configuration: 6x4
Shot Location: A.boni
Model of a mining excavator in front shovel configuration in scale 1:28.5. This 300 tonne machine is a representative of Liebherr's most popular size class and is ideally suited to load a fleet of 100 tonne payload mining trucks.
When LEGO introduced its 42100 Liebherr R 9800, I knew I had to get that set immediately after release. But I also knew from the beginning, that I would not like the official model's Technic design and that I had to build my own version.
Here it is, scaled larger than 42100, but on the other hand representing a much smaller machine than the 9800. About 300 vs. 800 tonnes in real life. This allowed me to use the main components of the official LEGO model to build my R 994 B. I used the clamshell bucket, the Power Functions XL actuators and the tracks and sprockets.
The main difference from 42100 lies in the electric components of my model. The following functions are all powered by two Power Functions rechargeable battery boxes and controlled by three SBricks via bluetooth connection and Brick Controller 2 app:
- Left and right crawler treads each using a Power Functions L motor
- Slewing of the upper structure using two Power Functions M motors
- Boom cylinders: one Power Functions XL motor
- Stick cylinders: one Power Functions L motor
- Bucket cylinders: one Power Functions M motor
- Clamshell bucket: one Brick Engine V1 motor (compatible to Power Functions)
- Access ladder: one Power Functions M motor
- Service flap: one Power Functions M motor
- Lighting: three pairs of Power Functions LEDs
Besides the main drive and digging functions, the model features a retractable access ladder and a lowerable service flap on the underside of the upper structure frame. The service flap is used to refuel and grease the excavator.
While building the Liebherr R 994 B Litronic in 1:28.5 scale, I could refer to a highly detailed diecast model of the very same machine in 1:50 scale.
Truck Manufacturer: MAN Truck & Bus AG
Model: MAN TGA
Chassis 18.360
Engine:
Suspension:
Axle Configuration:4x2
Shot Location: A.boni
Company/Owner: KL CNGBus Transportation Corporation
Fleet/Bus Number: 817038
Classification: Air-conditioned Provincial Bus
Coachbuilder: (Suzhou) Higer Bus Company, Ltd.
Body Model: Higer KLQ6112H
Engine Model: Yuchai YC6L280-30 (L53SA)
Chassis Model: Higer KLQ6110SE3 (LKLR1HSG**B)
Transmission: 6-speed Manual Transmission
Suspension: Leaf Spring Suspension
Seating Configuration: 2×2
Seating Capacity: 49
Franchise route: Batangas City–Cubao (Quezon City) via EDSA, SLEX or Cubao (Quezon City)–Kalibo (Aklan)
Route: Araneta Terminal, Quezon City [AAT, QC]–Port of Batangas, Batangas City, Batangas [BAT, BA] via E2 (Skyway-Hillsborough–SLEX-Calamba–SLEX-Santo Tomas; STAR-Lipa–Batangas City) / N4 (Jose P. Laurel Highway)
Municipalities/cities passing: Lipa City and San Jose
Type of Operation: Provincial Operation Public Utility Bus (Regular Class)
Area of Operation: CALABARZON (Region IV-A)
Shot location: EDSA-Boni, Mandaluyong City
Date taken: May 15, 2018 (14:35H)
Notices:
* Please DON'T GRAB A PHOTO WITHOUT A PERMISSION. If you're going to GRAB IT, please give A CREDIT TO THE OWNER. Also, don't PRINT SCREEN my photos.
** If I have mistakes on the specifications, please comment in a good manner so that I can edit it immediately.
*** The specifications and routes (for provincial, inter-provincial, and city operation) mentioned above are subjected for verification and may be changed without prior notice.
**** The vehicle's registration plate(s), conduction sticker(s), and/or persons (if applicable) were pixelated/blurred to prevent any conflict with the photographer, the bus company and/or to the car owner for their security and/or privacy purposes. So, don't use their plate number, conduction sticker, and vehicle tag as an evidence for any incident. And, I have taken this photo for bus fanatics, bus enthusiasts, and bus lovers purposes.
Truck Manufacturer: MAN Truck & Bus AG
Model: TGA
Chassis: 18.360
Engine:
Suspension:
Axle Configuration: 4x2
Shot Location: A.boni
Santrans
Bus Number.: 2275
Body: Xiamen King Long United (King Long)
Model: King Long XMQ6119T
Chassis: LA6R1FSD
Engine: Nissan Diesel FE6TC-H
Seating Configuration:
Capacity:
Shot Location: Cubao
SIMPLE = T / file does conform to FITS standard
BITPIX = -32 / number of bits per data pixel
NAXIS = 3 / number of data axes
NAXIS1 = 8000 / length of data axis 1
NAXIS2 = 8400 / length of data axis 2
NAXIS3 = 3 / length of data axis 3
EXTEND = T / FITS dataset may contain extensions
COMMENT FITS (Flexible Image Transport System) format is defined in 'Astronomy
COMMENT and Astrophysics', volume 376, page 359; bibcode: 2001A&A...376..359H
BZERO = 0. / Offset data range to that of unsigned short
BSCALE = 1. / Default scaling factor
PROGRAM = 'Siril 1.4.1' / Software that created this HDU
FILENAME= 'f673n_sc04px10_fcorr_drc_sci.fits'
DATE = '2026-01-24T09:07:12' / UTC date that FITS file was created
IMAGETYP= 'EXT ' / Type of image
EXPTIME = 13333.3333333333 / [s] Exposure time duration
TELESCOP= 'HST ' / Telescope used to acquire this image
FILTER = 'mixed ' / Active filter name
XBINNING= 1 / Camera binning mode
YBINNING= 1 / Camera binning mode
INSTRUME= 'WFC3 ' / Instrument name
STACKCNT= 48 / Stack frames
LIVETIME= 40000. / [s] Exposure time after deadtime correction
EXPSTART= 56902.19517988 / [JD] Exposure start time (standard Julian date)
EXPEND = 56905.54330485 / [JD] Exposure end time (standard Julian date)
CTYPE1 = 'RA---TAN' / TAN (gnomic) projection
CTYPE2 = 'DEC--TAN' / TAN (gnomic) projection
CUNIT1 = 'deg ' / Unit of coordinates
CUNIT2 = 'deg ' / Unit of coordinates
EQUINOX = 2000. / Equatorial equinox
CRPIX1 = 4000. / Axis1 reference pixel
CRPIX2 = 4200. / Axis2 reference pixel
CRVAL1 = 274.721587 / [deg] Axis1 reference value
CRVAL2 = -13.841549 / [deg] Axis2 reference value
LONPOLE = 180. / Native longitude of celestial pole
CDELT1 = -1.11111750516744E-05 / [deg] X pixel size
CDELT2 = 1.11112569800879E-05 / [deg] Y pixel size
PC1_1 = 0.819146770676383 / Linear transformation matrix (1, 1)
PC1_2 = 0.573583967776692 / Linear transformation matrix (1, 2)
PC2_1 = -0.573569705598004 / Linear transformation matrix (2, 1)
PC2_2 = 0.8191567571718 / Linear transformation matrix (2, 2)
ORIGIN = 'NOAO-IRAF FITS Image Kernel July 2003' / FITS file originator
IRAF-TLM= '2014-10-20T16:19:08' / Time of last modification
FILETYPE= 'SCI ' / type of data found in data file
/ DATA DESCRIPTION KEYWORDS
ROOTNAME= 'f673n_sc04px10_fcorr_drc_sci.fits' / rootname of the observation set
PRIMESI = 'WFC3 ' / instrument designated as prime
/ TARGET INFORMATION
TARGNAME= 'LBN67-UVIS ' / proposer's target name
RA_TARG = 2.747104166667E+02 / right ascension of the target (deg) (J2000)
DEC_TARG= -1.382888888889E+01 / declination of the target (deg) (J2000)
/ PROPOSAL INFORMATION
PROPOSID= 13926 / PEP proposal identifier
LINENUM = '09.003 ' / proposal logsheet line number
PR_INV_L= 'Levay ' / last name of principal investigator
PR_INV_F= 'Zolt ' / first name of principal investigator
PR_INV_M= ' ' / middle name / initial of principal investigat
/ EXPOSURE INFORMATION
SUNANGLE= 111.761848 / angle between sun and V1 axis
MOONANGL= 16.728901 / angle between moon and V1 axis
FGSLOCK = 'FINE ' / commanded FGS lock (FINE,COARSE,GYROS,UNKNOWN)
GYROMODE= 'T' / number of gyros scheduled, T=3+OBAD
REFFRAME= 'ICRS ' / guide star catalog version
MTFLAG = ' ' / moving target flag; T if it is a moving target
TIME-OBS= '09:35:53' / UT time of start of observation (hh🇲🇲ss)
TEXPTIME= 14400.0
EXPFLAG = 'NORMAL ' / Exposure interruption indicator
QUALCOM1= ' '
QUALCOM2= ' '
QUALCOM3= ' '
QUALITY = ' '
DARKTIME= 903.843296 / fiducial pixel dark time (secs)
/ POINTING INFORMATION
PA_V3 = 280.000702 / position angle of V3-axis of HST (deg)
/ TARGET OFFSETS (POSTARGS)
/ DIAGNOSTIC KEYWORDS
OPUS_VER= 'OPUS 2014_2 ' / OPUS software system version number
CAL_VER = '3.1.6(15-Nov-2013)' / CALWF3 code version
PROCTIME= 5.690858548611E+04 / Pipeline processing time (MJD)
/ SCIENCE INSTRUMENT CONFIGURATION
OBSTYPE = 'IMAGING ' / observation type - imaging or spectroscopic
OBSMODE = 'ACCUM ' / operating mode
CTEIMAGE= ' ' / type of Charge Transfer Image, if applicable
SCLAMP = 'NONE ' / lamp status, NONE or name of lamp which is on
NRPTEXP = 1 / number of repeat exposures in set: default 1
SUBARRAY= F / data from a subarray (T) or full frame (F)
DETECTOR= 'UVIS' / detector in use: UVIS or IR
PROPAPER= ' ' / proposed aperture name
DIRIMAGE= 'NONE ' / direct image for grism or prism exposure
CTEDIR = 'NONE ' / CTE measurement direction: serial or parallel
CRSPLIT = 1 / number of cosmic ray split exposures
/ CALIBRATION SWITCHES: PERFORM, OMIT, COMPLETE, SKIPPED
WRTERR = T / write out error array extension
DQICORR = 'COMPLETE' / data quality initialization
ATODCORR= 'OMIT ' / correct for A to D conversion errors
BLEVCORR= 'COMPLETE' / subtract bias level computed from overscan
BIASCORR= 'COMPLETE' / Subtract bias image
FLSHCORR= 'OMIT ' / post flash correction
CRCORR = 'OMIT ' / combine observations to reject cosmic rays
EXPSCORR= 'COMPLETE' / process individual observations after cr-reject
SHADCORR= 'OMIT ' / apply shutter shading correction
DARKCORR= 'COMPLETE' / Subtract dark image
FLATCORR= 'COMPLETE' / flat field data
PHOTCORR= 'COMPLETE' / populate photometric header keywords
DRIZCORR= 'COMPLETE' / drizzle processing
/ CALIBRATION REFERENCE FILES
BPIXTAB = 'iref$u5d2012li_bpx.fits' / bad pixel table
CCDTAB = 'iref$t291659mi_ccd.fits' / detector calibration parameters
ATODTAB = 'N/A ' / analog to digital correction file
OSCNTAB = 'iref$q911321oi_osc.fits' / detector overscan table
BIASFILE= 'iref$v5j1716ei_bia.fits' / bias image file name
FLSHFILE= 'N/A ' / post flash correction file name
CRREJTAB= 'iref$n9i1435li_crr.fits' / cosmic ray rejection parameters
SHADFILE= 'N/A ' / shutter shading correction file
DARKFILE= 'MULTIPLE' / dark image file name
PFLTFILE= 'iref$vcd2018mi_pfl.fits' / pixel to pixel flat field file name
DFLTFILE= 'N/A ' / delta flat field file name
LFLTFILE= 'N/A ' / low order flat
GRAPHTAB= 'mtab$xb615138m_tmg.fits' / the HST graph table
COMPTAB = 'mtab$y482015bm_tmc.fits' / the HST components table
IMPHTTAB= 'iref$x5h1320fi_imp.fits' / Image Photometry Table
IDCTAB = 'iref$x5h1320ei_idc.fits' / image distortion correction table
DGEOFILE= 'N/A ' / Distortion correction image
MDRIZTAB= 'iref$ubi1853qi_mdz.fits' / MultiDrizzle parameter table
D2IMFILE= 'iref$x5o1555ji_d2i.fits' / Column Correction Reference File
/ COSMIC RAY REJECTION ALGORITHM PARAMETERS
MEANEXP = 0.0 / reference exposure time for parameters
SCALENSE= 0.0 / multiplicative scale factor applied to noise
INITGUES= ' ' / initial guess method (MIN or MED)
CRSIGMAS= ' ' / statistical rejection criteria
CRRADIUS= 0.0 / rejection propagation radius (pixels)
CRTHRESH= 0.000000 / rejection propagation threshold
BADINPDQ= 0 / data quality flag bits to reject
CRMASK = F / flag CR-rejected pixels in input files (T/F)
/ POST FLASH PARAMETERS
FLASHDUR= 0.0 / Exposure time in seconds: 0.1 to 409.5
FLASHCUR= 'ZERO ' / Post flash current (zero, low, medium, high)
FLASHLVL= 0 / Post flash requested flash level
FLASHSTA= 'NOT PERFORMED ' / Status: SUCCESSFUL, ABORTED, NOT PERFORMED
/ CHARGE INJECTION PARAMETERS
CHINJECT= 'NONE ' / Charge Injection Mode
/ OTFR KEYWORDS
T_SGSTAR= 'MULTIPLE' / OMS calculated guide star control
/ PATTERN KEYWORDS
PATTERN1= 'MULTIPLE' / primary pattern type
P1_SHAPE= 'LINE ' / primary pattern shape
P1_PURPS= 'MULTIPLE' / primary pattern purpose
P1_NPTS = 2 / number of points in primary pattern
P1_PSPAC= 12.0 / point spacing for primary pattern (arc-sec)
P1_LSPAC= 0.000000 / line spacing for primary pattern (arc-sec)
P1_ANGLE= 0.000000 / angle between sides of parallelogram patt (deg)
P1_FRAME= 'POS-TARG ' / coordinate frame of primary pattern
P1_ORINT= 65.0 / orientation of pattern to coordinate frame (deg
P1_CENTR= 'NO ' / center pattern relative to pointing (yes/no)
PATTSTEP= 2 / position number of this point in the pattern
/ ENGINEERING PARAMETERS
CCDAMP = 'ABCD' / CCD Amplifier Readout Configuration
CCDGAIN = 1.5 / commanded gain of CCD
CCDOFSTA= 3 / commanded CCD bias offset for amplifier A
CCDOFSTB= 3 / commanded CCD bias offset for amplifier B
CCDOFSTC= 3 / commanded CCD bias offset for amplifier C
CCDOFSTD= 3 / commanded CCD bias offset for amplifier D
/ CALIBRATED ENGINEERING PARAMETERS
ATODGNA = 1.5599999E+00 / calibrated gain for amplifier A
ATODGNB = 1.5599999E+00 / calibrated gain for amplifier B
ATODGNC = 1.5599999E+00 / calibrated gain for amplifier C
ATODGND = 1.5599999E+00 / calibrated gain for amplifier D
READNSEA= 3.0300000E+00 / calibrated read noise for amplifier A
READNSEB= 3.1300001E+00 / calibrated read noise for amplifier B
READNSEC= 3.0799999E+00 / calibrated read noise for amplifier C
READNSED= 3.1800001E+00 / calibrated read noise for amplifier D
BIASLEVA= 2.5552041E+03 / bias level for amplifier A
BIASLEVB= 2.5425671E+03 / bias level for amplifier B
BIASLEVC= 2.5028616E+03 / bias level for amplifier C
BIASLEVD= 2.6044766E+03 / bias level for amplifier D
/ ASSOCIATION KEYWORDS
ASN_ID = 'ICK909050 ' / unique identifier assigned to association
ASN_TAB = 'MULTIPLE' / name of the association table
ASN_MTYP= 'PROD-DTH' / Role of the Member in the Association
CRDS_CTX= 'hst_0277.pmap'
DISTNAME= 'ick909d3q_x5h1320ei-NOMODEL-x5o1555ji'
SIPNAME = 'ick909d3q_x5h1320ei'
UPWCSVER= '1.2.1.dev33816' / Version of STWCS used to updated the WCS
PYWCSVER= '0.4 ' / Version of PYWCS used to updated the WCS
RULESVER= 1.1 / Version ID for header kw rules file
BLENDVER= '1.1.0 ' / Version of blendheader software used
RULEFILE= '/usr/stsci/ssbx/python/lib/python2.7/site-packages/fitsblender-0.2.&'
CONTINUE '5.dev34878-py2.7.egg/fitsblender/wfc3_header.rules&'
CONTINUE '&' / Name of header kw rules file
NDRIZIM = 32 / Drizzle, No. images drizzled onto output
D001OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D001VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D001SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D001COEF= 'SIP ' / Drizzle, source of coefficients
D001OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D001OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D001WTSC= 1 / Drizzle, weighting factor for input image
D001MASK= 'fck905k8q_sci1_final_mask.fits' / Drizzle, input weighting image
D001FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D001WKEY= '' / Input image WCS Version used
D001OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D001KERN= 'square ' / Drizzle, form of weight distribution kernel
D001GEOM= 'wcs ' / Drizzle, source of geometric information
D001ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D001PIXF= 1.0 / Drizzle, linear size of drop
D001DATA= 'fck905k8q_flc.fits[sci,1]' / Drizzle, input data image
D001DEXP= 900.0 / Drizzle, input image exposure time (s)
D002OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D002VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D002SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D002COEF= 'SIP ' / Drizzle, source of coefficients
D002OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D002OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D002WTSC= 1 / Drizzle, weighting factor for input image
D002MASK= 'fck905k8q_sci2_final_mask.fits' / Drizzle, input weighting image
D002FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D002WKEY= '' / Input image WCS Version used
D002OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D002KERN= 'square ' / Drizzle, form of weight distribution kernel
D002GEOM= 'wcs ' / Drizzle, source of geometric information
D002ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D002PIXF= 1.0 / Drizzle, linear size of drop
D002DATA= 'fck905k8q_flc.fits[sci,2]' / Drizzle, input data image
D002DEXP= 900.0 / Drizzle, input image exposure time (s)
D003OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D003VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D003SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D003COEF= 'SIP ' / Drizzle, source of coefficients
D003OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D003OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D003WTSC= 1 / Drizzle, weighting factor for input image
D003MASK= 'fck905khq_sci1_final_mask.fits' / Drizzle, input weighting image
D003FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D003WKEY= '' / Input image WCS Version used
D003OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D003KERN= 'square ' / Drizzle, form of weight distribution kernel
D003GEOM= 'wcs ' / Drizzle, source of geometric information
D003ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D003PIXF= 1.0 / Drizzle, linear size of drop
D003DATA= 'fck905khq_flc.fits[sci,1]' / Drizzle, input data image
D003DEXP= 900.0 / Drizzle, input image exposure time (s)
D004OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D004VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D004SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D004COEF= 'SIP ' / Drizzle, source of coefficients
D004OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D004OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D004WTSC= 1 / Drizzle, weighting factor for input image
D004MASK= 'fck905khq_sci2_final_mask.fits' / Drizzle, input weighting image
D004FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D004WKEY= '' / Input image WCS Version used
D004OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D004KERN= 'square ' / Drizzle, form of weight distribution kernel
D004GEOM= 'wcs ' / Drizzle, source of geometric information
D004ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D004PIXF= 1.0 / Drizzle, linear size of drop
D004DATA= 'fck905khq_flc.fits[sci,2]' / Drizzle, input data image
D004DEXP= 900.0 / Drizzle, input image exposure time (s)
D005OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D005VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D005SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D005COEF= 'SIP ' / Drizzle, source of coefficients
D005OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D005OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D005WTSC= 1 / Drizzle, weighting factor for input image
D005MASK= 'fck905kqq_sci1_final_mask.fits' / Drizzle, input weighting image
D005FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D005WKEY= '' / Input image WCS Version used
D005OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D005KERN= 'square ' / Drizzle, form of weight distribution kernel
D005GEOM= 'wcs ' / Drizzle, source of geometric information
D005ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D005PIXF= 1.0 / Drizzle, linear size of drop
D005DATA= 'fck905kqq_flc.fits[sci,1]' / Drizzle, input data image
D005DEXP= 900.0 / Drizzle, input image exposure time (s)
D006OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D006VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D006SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D006COEF= 'SIP ' / Drizzle, source of coefficients
D006OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D006OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D006WTSC= 1 / Drizzle, weighting factor for input image
D006MASK= 'fck905kqq_sci2_final_mask.fits' / Drizzle, input weighting image
D006FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D006WKEY= '' / Input image WCS Version used
D006OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D006KERN= 'square ' / Drizzle, form of weight distribution kernel
D006GEOM= 'wcs ' / Drizzle, source of geometric information
D006ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D006PIXF= 1.0 / Drizzle, linear size of drop
D006DATA= 'fck905kqq_flc.fits[sci,2]' / Drizzle, input data image
D006DEXP= 900.0 / Drizzle, input image exposure time (s)
D007OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D007VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D007SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D007COEF= 'SIP ' / Drizzle, source of coefficients
D007OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D007OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D007WTSC= 1 / Drizzle, weighting factor for input image
D007MASK= 'fck906kzq_sci1_final_mask.fits' / Drizzle, input weighting image
D007FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D007WKEY= '' / Input image WCS Version used
D007OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D007KERN= 'square ' / Drizzle, form of weight distribution kernel
D007GEOM= 'wcs ' / Drizzle, source of geometric information
D007ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D007PIXF= 1.0 / Drizzle, linear size of drop
D007DATA= 'fck906kzq_flc.fits[sci,1]' / Drizzle, input data image
D007DEXP= 900.0 / Drizzle, input image exposure time (s)
D008OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D008VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D008SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D008COEF= 'SIP ' / Drizzle, source of coefficients
D008OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D008OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D008WTSC= 1 / Drizzle, weighting factor for input image
D008MASK= 'fck906kzq_sci2_final_mask.fits' / Drizzle, input weighting image
D008FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D008WKEY= '' / Input image WCS Version used
D008OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D008KERN= 'square ' / Drizzle, form of weight distribution kernel
D008GEOM= 'wcs ' / Drizzle, source of geometric information
D008ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D008PIXF= 1.0 / Drizzle, linear size of drop
D008DATA= 'fck906kzq_flc.fits[sci,2]' / Drizzle, input data image
D008DEXP= 900.0 / Drizzle, input image exposure time (s)
D009OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D009VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D009SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D009COEF= 'SIP ' / Drizzle, source of coefficients
D009OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D009OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D009WTSC= 1 / Drizzle, weighting factor for input image
D009MASK= 'fck906l8q_sci1_final_mask.fits' / Drizzle, input weighting image
D009FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D009WKEY= '' / Input image WCS Version used
D009OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D009KERN= 'square ' / Drizzle, form of weight distribution kernel
D009GEOM= 'wcs ' / Drizzle, source of geometric information
D009ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D009PIXF= 1.0 / Drizzle, linear size of drop
D009DATA= 'fck906l8q_flc.fits[sci,1]' / Drizzle, input data image
D009DEXP= 900.0 / Drizzle, input image exposure time (s)
D010OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D010VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D010SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D010COEF= 'SIP ' / Drizzle, source of coefficients
D010OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D010OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D010WTSC= 1 / Drizzle, weighting factor for input image
D010MASK= 'fck906l8q_sci2_final_mask.fits' / Drizzle, input weighting image
D010FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D010WKEY= '' / Input image WCS Version used
D010OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D010KERN= 'square ' / Drizzle, form of weight distribution kernel
D010GEOM= 'wcs ' / Drizzle, source of geometric information
D010ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D010PIXF= 1.0 / Drizzle, linear size of drop
D010DATA= 'fck906l8q_flc.fits[sci,2]' / Drizzle, input data image
D010DEXP= 900.0 / Drizzle, input image exposure time (s)
D011OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D011VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D011SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D011COEF= 'SIP ' / Drizzle, source of coefficients
D011OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D011OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D011WTSC= 1 / Drizzle, weighting factor for input image
D011MASK= 'fck906lhq_sci1_final_mask.fits' / Drizzle, input weighting image
D011FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D011WKEY= '' / Input image WCS Version used
D011OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D011KERN= 'square ' / Drizzle, form of weight distribution kernel
D011GEOM= 'wcs ' / Drizzle, source of geometric information
D011ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D011PIXF= 1.0 / Drizzle, linear size of drop
D011DATA= 'fck906lhq_flc.fits[sci,1]' / Drizzle, input data image
D011DEXP= 900.0 / Drizzle, input image exposure time (s)
D012OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D012VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D012SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D012COEF= 'SIP ' / Drizzle, source of coefficients
D012OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D012OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D012WTSC= 1 / Drizzle, weighting factor for input image
D012MASK= 'fck906lhq_sci2_final_mask.fits' / Drizzle, input weighting image
D012FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D012WKEY= '' / Input image WCS Version used
D012OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D012KERN= 'square ' / Drizzle, form of weight distribution kernel
D012GEOM= 'wcs ' / Drizzle, source of geometric information
D012ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D012PIXF= 1.0 / Drizzle, linear size of drop
D012DATA= 'fck906lhq_flc.fits[sci,2]' / Drizzle, input data image
D012DEXP= 900.0 / Drizzle, input image exposure time (s)
D013OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D013VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D013SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D013COEF= 'SIP ' / Drizzle, source of coefficients
D013OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D013OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D013WTSC= 1 / Drizzle, weighting factor for input image
D013MASK= 'fck907nnq_sci1_final_mask.fits' / Drizzle, input weighting image
D013FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D013WKEY= '' / Input image WCS Version used
D013OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D013KERN= 'square ' / Drizzle, form of weight distribution kernel
D013GEOM= 'wcs ' / Drizzle, source of geometric information
D013ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D013PIXF= 1.0 / Drizzle, linear size of drop
D013DATA= 'fck907nnq_flc.fits[sci,1]' / Drizzle, input data image
D013DEXP= 900.0 / Drizzle, input image exposure time (s)
D014OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D014VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D014SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D014COEF= 'SIP ' / Drizzle, source of coefficients
D014OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D014OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D014WTSC= 1 / Drizzle, weighting factor for input image
D014MASK= 'fck907nnq_sci2_final_mask.fits' / Drizzle, input weighting image
D014FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D014WKEY= '' / Input image WCS Version used
D014OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D014KERN= 'square ' / Drizzle, form of weight distribution kernel
D014GEOM= 'wcs ' / Drizzle, source of geometric information
D014ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D014PIXF= 1.0 / Drizzle, linear size of drop
D014DATA= 'fck907nnq_flc.fits[sci,2]' / Drizzle, input data image
D014DEXP= 900.0 / Drizzle, input image exposure time (s)
D015OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D015VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D015SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D015COEF= 'SIP ' / Drizzle, source of coefficients
D015OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D015OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D015WTSC= 1 / Drizzle, weighting factor for input image
D015MASK= 'fck907o4q_sci1_final_mask.fits' / Drizzle, input weighting image
D015FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D015WKEY= '' / Input image WCS Version used
D015OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D015KERN= 'square ' / Drizzle, form of weight distribution kernel
D015GEOM= 'wcs ' / Drizzle, source of geometric information
D015ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D015PIXF= 1.0 / Drizzle, linear size of drop
D015DATA= 'fck907o4q_flc.fits[sci,1]' / Drizzle, input data image
D015DEXP= 900.0 / Drizzle, input image exposure time (s)
D016OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D016VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D016SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D016COEF= 'SIP ' / Drizzle, source of coefficients
D016OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D016OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D016WTSC= 1 / Drizzle, weighting factor for input image
D016MASK= 'fck907o4q_sci2_final_mask.fits' / Drizzle, input weighting image
D016FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D016WKEY= '' / Input image WCS Version used
D016OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D016KERN= 'square ' / Drizzle, form of weight distribution kernel
D016GEOM= 'wcs ' / Drizzle, source of geometric information
D016ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D016PIXF= 1.0 / Drizzle, linear size of drop
D016DATA= 'fck907o4q_flc.fits[sci,2]' / Drizzle, input data image
D016DEXP= 900.0 / Drizzle, input image exposure time (s)
D017OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D017VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D017SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D017COEF= 'SIP ' / Drizzle, source of coefficients
D017OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D017OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D017WTSC= 1 / Drizzle, weighting factor for input image
D017MASK= 'fck907oxq_sci1_final_mask.fits' / Drizzle, input weighting image
D017FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D017WKEY= '' / Input image WCS Version used
D017OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D017KERN= 'square ' / Drizzle, form of weight distribution kernel
D017GEOM= 'wcs ' / Drizzle, source of geometric information
D017ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D017PIXF= 1.0 / Drizzle, linear size of drop
D017DATA= 'fck907oxq_flc.fits[sci,1]' / Drizzle, input data image
D017DEXP= 900.0 / Drizzle, input image exposure time (s)
D018OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D018VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D018SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D018COEF= 'SIP ' / Drizzle, source of coefficients
D018OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D018OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D018WTSC= 1 / Drizzle, weighting factor for input image
D018MASK= 'fck907oxq_sci2_final_mask.fits' / Drizzle, input weighting image
D018FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D018WKEY= '' / Input image WCS Version used
D018OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D018KERN= 'square ' / Drizzle, form of weight distribution kernel
D018GEOM= 'wcs ' / Drizzle, source of geometric information
D018ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D018PIXF= 1.0 / Drizzle, linear size of drop
D018DATA= 'fck907oxq_flc.fits[sci,2]' / Drizzle, input data image
D018DEXP= 900.0 / Drizzle, input image exposure time (s)
D019OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D019VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D019SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D019COEF= 'SIP ' / Drizzle, source of coefficients
D019OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D019OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D019WTSC= 1 / Drizzle, weighting factor for input image
D019MASK= 'fck908peq_sci1_final_mask.fits' / Drizzle, input weighting image
D019FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D019WKEY= '' / Input image WCS Version used
D019OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D019KERN= 'square ' / Drizzle, form of weight distribution kernel
D019GEOM= 'wcs ' / Drizzle, source of geometric information
D019ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D019PIXF= 1.0 / Drizzle, linear size of drop
D019DATA= 'fck908peq_flc.fits[sci,1]' / Drizzle, input data image
D019DEXP= 900.0 / Drizzle, input image exposure time (s)
D020OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D020VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D020SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D020COEF= 'SIP ' / Drizzle, source of coefficients
D020OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D020OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D020WTSC= 1 / Drizzle, weighting factor for input image
D020MASK= 'fck908peq_sci2_final_mask.fits' / Drizzle, input weighting image
D020FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D020WKEY= '' / Input image WCS Version used
D020OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D020KERN= 'square ' / Drizzle, form of weight distribution kernel
D020GEOM= 'wcs ' / Drizzle, source of geometric information
D020ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D020PIXF= 1.0 / Drizzle, linear size of drop
D020DATA= 'fck908peq_flc.fits[sci,2]' / Drizzle, input data image
D020DEXP= 900.0 / Drizzle, input image exposure time (s)
D021OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D021VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D021SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D021COEF= 'SIP ' / Drizzle, source of coefficients
D021OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D021OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D021WTSC= 1 / Drizzle, weighting factor for input image
D021MASK= 'fck908pnq_sci1_final_mask.fits' / Drizzle, input weighting image
D021FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D021WKEY= '' / Input image WCS Version used
D021OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D021KERN= 'square ' / Drizzle, form of weight distribution kernel
D021GEOM= 'wcs ' / Drizzle, source of geometric information
D021ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D021PIXF= 1.0 / Drizzle, linear size of drop
D021DATA= 'fck908pnq_flc.fits[sci,1]' / Drizzle, input data image
D021DEXP= 900.0 / Drizzle, input image exposure time (s)
D022OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D022VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D022SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D022COEF= 'SIP ' / Drizzle, source of coefficients
D022OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D022OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D022WTSC= 1 / Drizzle, weighting factor for input image
D022MASK= 'fck908pnq_sci2_final_mask.fits' / Drizzle, input weighting image
D022FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D022WKEY= '' / Input image WCS Version used
D022OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D022KERN= 'square ' / Drizzle, form of weight distribution kernel
D022GEOM= 'wcs ' / Drizzle, source of geometric information
D022ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D022PIXF= 1.0 / Drizzle, linear size of drop
D022DATA= 'fck908pnq_flc.fits[sci,2]' / Drizzle, input data image
D022DEXP= 900.0 / Drizzle, input image exposure time (s)
D023OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D023VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D023SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D023COEF= 'SIP ' / Drizzle, source of coefficients
D023OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D023OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D023WTSC= 1 / Drizzle, weighting factor for input image
D023MASK= 'fck908pwq_sci1_final_mask.fits' / Drizzle, input weighting image
D023FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D023WKEY= '' / Input image WCS Version used
D023OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D023KERN= 'square ' / Drizzle, form of weight distribution kernel
D023GEOM= 'wcs ' / Drizzle, source of geometric information
D023ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D023PIXF= 1.0 / Drizzle, linear size of drop
D023DATA= 'fck908pwq_flc.fits[sci,1]' / Drizzle, input data image
D023DEXP= 900.0 / Drizzle, input image exposure time (s)
D024OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D024VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D024SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D024COEF= 'SIP ' / Drizzle, source of coefficients
D024OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D024OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D024WTSC= 1 / Drizzle, weighting factor for input image
D024MASK= 'fck908pwq_sci2_final_mask.fits' / Drizzle, input weighting image
D024FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D024WKEY= '' / Input image WCS Version used
D024OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D024KERN= 'square ' / Drizzle, form of weight distribution kernel
D024GEOM= 'wcs ' / Drizzle, source of geometric information
D024ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D024PIXF= 1.0 / Drizzle, linear size of drop
D024DATA= 'fck908pwq_flc.fits[sci,2]' / Drizzle, input data image
D024DEXP= 900.0 / Drizzle, input image exposure time (s)
D025OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D025VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D025SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D025COEF= 'SIP ' / Drizzle, source of coefficients
D025OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D025OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D025WTSC= 1 / Drizzle, weighting factor for input image
D025MASK= 'fck909c6q_sci1_final_mask.fits' / Drizzle, input weighting image
D025FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D025WKEY= '' / Input image WCS Version used
D025OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D025KERN= 'square ' / Drizzle, form of weight distribution kernel
D025GEOM= 'wcs ' / Drizzle, source of geometric information
D025ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D025PIXF= 1.0 / Drizzle, linear size of drop
D025DATA= 'fck909c6q_flc.fits[sci,1]' / Drizzle, input data image
D025DEXP= 900.0 / Drizzle, input image exposure time (s)
D026OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D026VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D026SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D026COEF= 'SIP ' / Drizzle, source of coefficients
D026OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D026OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D026WTSC= 1 / Drizzle, weighting factor for input image
D026MASK= 'fck909c6q_sci2_final_mask.fits' / Drizzle, input weighting image
D026FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D026WKEY= '' / Input image WCS Version used
D026OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D026KERN= 'square ' / Drizzle, form of weight distribution kernel
D026GEOM= 'wcs ' / Drizzle, source of geometric information
D026ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D026PIXF= 1.0 / Drizzle, linear size of drop
D026DATA= 'fck909c6q_flc.fits[sci,2]' / Drizzle, input data image
D026DEXP= 900.0 / Drizzle, input image exposure time (s)
D027OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D027VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D027SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D027COEF= 'SIP ' / Drizzle, source of coefficients
D027OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D027OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D027WTSC= 1 / Drizzle, weighting factor for input image
D027MASK= 'fck909d3q_sci1_final_mask.fits' / Drizzle, input weighting image
D027FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D027WKEY= '' / Input image WCS Version used
D027OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D027KERN= 'square ' / Drizzle, form of weight distribution kernel
D027GEOM= 'wcs ' / Drizzle, source of geometric information
D027ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D027PIXF= 1.0 / Drizzle, linear size of drop
D027DATA= 'fck909d3q_flc.fits[sci,1]' / Drizzle, input data image
D027DEXP= 900.0 / Drizzle, input image exposure time (s)
D028OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D028VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D028SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D028COEF= 'SIP ' / Drizzle, source of coefficients
D028OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D028OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D028WTSC= 1 / Drizzle, weighting factor for input image
D028MASK= 'fck909d3q_sci2_final_mask.fits' / Drizzle, input weighting image
D028FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D028WKEY= '' / Input image WCS Version used
D028OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D028KERN= 'square ' / Drizzle, form of weight distribution kernel
D028GEOM= 'wcs ' / Drizzle, source of geometric information
D028ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D028PIXF= 1.0 / Drizzle, linear size of drop
D028DATA= 'fck909d3q_flc.fits[sci,2]' / Drizzle, input data image
D028DEXP= 900.0 / Drizzle, input image exposure time (s)
D029OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D029VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D029SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D029COEF= 'SIP ' / Drizzle, source of coefficients
D029OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D029OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D029WTSC= 1 / Drizzle, weighting factor for input image
D029MASK= 'fck910dcq_sci1_final_mask.fits' / Drizzle, input weighting image
D029FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D029WKEY= '' / Input image WCS Version used
D029OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D029KERN= 'square ' / Drizzle, form of weight distribution kernel
D029GEOM= 'wcs ' / Drizzle, source of geometric information
D029ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D029PIXF= 1.0 / Drizzle, linear size of drop
D029DATA= 'fck910dcq_flc.fits[sci,1]' / Drizzle, input data image
D029DEXP= 900.0 / Drizzle, input image exposure time (s)
D030OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D030VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D030SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D030COEF= 'SIP ' / Drizzle, source of coefficients
D030OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D030OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D030WTSC= 1 / Drizzle, weighting factor for input image
D030MASK= 'fck910dcq_sci2_final_mask.fits' / Drizzle, input weighting image
D030FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D030WKEY= '' / Input image WCS Version used
D030OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D030KERN= 'square ' / Drizzle, form of weight distribution kernel
D030GEOM= 'wcs ' / Drizzle, source of geometric information
D030ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D030PIXF= 1.0 / Drizzle, linear size of drop
D030DATA= 'fck910dcq_flc.fits[sci,2]' / Drizzle, input data image
D030DEXP= 900.0 / Drizzle, input image exposure time (s)
D031OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D031VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D031SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D031COEF= 'SIP ' / Drizzle, source of coefficients
D031OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D031OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D031WTSC= 1 / Drizzle, weighting factor for input image
D031MASK= 'fck910dlq_sci1_final_mask.fits' / Drizzle, input weighting image
D031FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D031WKEY= '' / Input image WCS Version used
D031OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D031KERN= 'square ' / Drizzle, form of weight distribution kernel
D031GEOM= 'wcs ' / Drizzle, source of geometric information
D031ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D031PIXF= 1.0 / Drizzle, linear size of drop
D031DATA= 'fck910dlq_flc.fits[sci,1]' / Drizzle, input data image
D031DEXP= 900.0 / Drizzle, input image exposure time (s)
D032OUDA= 'f673n_sc04px10_fcorr_drc.fits' / Drizzle, output data image
D032VER = 'Callable C-based DRIZZLE Version 0.8 (20th M' / Drizzle, task version
D032SCAL= 0.03999999999639195 / Drizzle, pixel size (arcsec) of output image
D032COEF= 'SIP ' / Drizzle, source of coefficients
D032OUWE= 'f673n_sc04px10_fcorr_drc_wht.fits' / Drizzle, output weighting image
D032OUCO= 'f673n_sc04px10_fcorr_drc_ctx.fits' / Drizzle, output context image
D032WTSC= 1 / Drizzle, weighting factor for input image
D032MASK= 'fck910dlq_sci2_final_mask.fits' / Drizzle, input weighting image
D032FVAL= 'INDEF ' / Drizzle, fill value for zero weight output pix
D032WKEY= '' / Input image WCS Version used
D032OUUN= 'cps ' / Drizzle, units of output image - counts or cps
D032KERN= 'square ' / Drizzle, form of weight distribution kernel
D032GEOM= 'wcs ' / Drizzle, source of geometric information
D032ISCL= 0.03962 / Drizzle, default IDCTAB pixel size(arcsec)
D032PIXF= 1.0 / Drizzle, linear size of drop
D032DATA= 'fck910dlq_flc.fits[sci,2]' / Drizzle, input data image
D032DEXP= 900.0 / Drizzle, input image exposure time (s)
EXPNAME = 'ick905k8q ' / exposure identifier
BUNIT = 'ELECTRONS/S' / Units of science product
CCDCHIP = '-999 ' / CCD chip (1 or 2)
ORIENTAT= -35.00000010001074 / position angle of image y axis (deg. e of n)
VAFACTOR= 1.0
LTV1 = 0.0000000E+00 / offset in X to subsection start
LTV2 = 0.0000000E+00 / offset in Y to subsection start
LTM1_1 = 1.0 / reciprocal of sampling rate in X
LTM2_2 = 1.0 / reciprocal of sampling rate in Y
PA_APER = -35.1623 / Position Angle of reference aperture center (de
RA_APER = 2.746828894131E+02 / RA of aperture reference position
DEC_APER= -1.382248339952E+01 / Declination of aperture reference position
PHOTMODE= 'WFC3 UVIS2 F673N CAL' / observation con
PHOTFLAM= 2.23971949999999E-18 / inverse sensitivity, ergs/cm2/Ang/electron
PHOTFNU = 3.41999895E-06 / inverse sensitivity, Jy*sec/electron
PHOTZPT = -21.10000000000001 / ST magnitude zero point
PHOTPLAM= 6765.915800000002 / Pivot wavelength (Angstroms)
PHOTBW = 41.99599850000001 / RMS bandwidth of filter plus detector
CENTERA1= 2104 / subarray axis1 center pt in unbinned dect. pix
CENTERA2= 1036 / subarray axis2 center pt in unbinned dect. pix
SIZAXIS1= 4096 / subarray axis1 size in unbinned detector pixels
SIZAXIS2= 2051 / subarray axis2 size in unbinned detector pixels
BINAXIS1= 1 / axis1 data bin size in unbinned detector pixels
BINAXIS2= 1 / axis2 data bin size in unbinned detector pixels
PODPSFF = F / podps fill present (T/F)
STDCFFF = F / science telemetry fill data present (T=1/F=0)
STDCFFP = '0x5569' / science telemetry fill pattern (hex)
SDQFLAGS= 31743 / serious data quality flags
SOFTERRS= 0 / number of soft error pixels (DQF=1)
MEANFLSH= 0.000000 / Mean number of counts in post flash exposure
D2IM1 = 'EXTVER: 1' / Version number of WCSDVARR extension containing d2im loo
D2IM1 = 'NAXES: 2' / Number of independent variables in d2im function
D2IM1 = 'AXIS.1: 1' / Axis number of the jth independent variable in a d2im fu
D2IM1 = 'AXIS.2: 2' / Axis number of the jth independent variable in a d2im fu
D2IM2 = 'EXTVER: 2' / Version number of WCSDVARR extension containing d2im loo
D2IM2 = 'NAXES: 2' / Number of independent variables in d2im function
D2IM2 = 'AXIS.1: 1' / Axis number of the jth independent variable in a d2im fu
D2IM2 = 'AXIS.2: 2' / Axis number of the jth independent variable in a d2im fu
RESTFRQO= 0
RESTWAVO= 0
END
Royal Cargo
Truck Manufacturer: MAN Truck & Bus AG
Model: CLA
Chassis: 26.280
Engine:
Suspension:
Axle Configuration: 6x4
Truck Manufacturer: MAN Truck & Bus AG
Model: TGA
Chassis: 24.390
Trailer:
Engine:
Suspension:
Axle Configuration: 6x2*4 Midlift
Trailer: 3 Axle Flammable Tanker Transbuilt
Shot Location: Balintawak
Commentary.
Ocean, land, harbour – an unusual configuration.
The geology of south-west Argyll provides a series of land-protected harbours and ideal sailing waters.
Therefore, this ancient but mellow coastline of Dalriada is a mecca for yachting marinas.
In this scene, looking North-West, Tayvallich is one of very few east-facing villages on the majestic western seaboard.
A strip of land shelters the multifarious blue, yellow, white and red craft from the Atlantic elements.
Uncommercialised, unspoilt Tayvallich is charming, under-stated and wonderfully modest, in my opinion.
Loch Melfort, Crinan, Tayvallich, Ardfern and Craobh Haven are hidden jewels in an immensely fractured, twisting and convoluted coastline.
With island vistas and visits to Islay, Jura, Scarba, Luing, Seil, Kerrera and Lismore these cosy, calm and peaceful harbours
act as perfect sanctuaries to the incredible sea-kingdom of Dalriada.
It is not unusual on the West Coast and Hebrides for cows to outnumber tourists on the shoreline.
Wise cows.
Lucky cows.
And lucky me!
Commuters Bus Corporation
Bus Number: 06520
Classification: Non Airconditioned - City Operation Bus
Coachbuilder: Almazora Motors Corp.
Model: AMC City Star FV
Suspension: Leaf Spring Suspension
Chassis: Isuzu PABFVR34SLQ
Engine: Isuzu 6HK1-TCN
Seating Configuration : 2x3
Capacity:
Shot Location: Kamias
“Illustration of an aerospace vehicle which incorporates an aero-electric propulsion system features circular disk configuration.”
The above, and all following, taken from “Ryan Reporter”, VOL. 23, FEB., 1962, NO. 1:
“ELECTRICITY for SPACE EXPLORATION
"I have produced electrical discharges the actual path of which, from end to end, was probably more than one hundred feet long; but it would not be difficult to reach
lengths one hundred times as great.
"I have produced electrical movements occurring at the rate of approximately 100,000 horsepower, but rates of 1-, 5- or 10,000,000 horsepower are easily practicable.
"Instead of sending sound-vibrations toward a distant wall, I have sent electrical vibrations toward the remote boundaries of the earth, and instead of the wall the earth has replied. In place of an echo I have obtained a stationary electrical wave, a wave reflected from afar.
"My measurements and calculations have shown that it is perfectly practicable to produce on our globe, by the use of these principles, an electric movement of such magnitude that, without the slightest doubt, its effect will be perceptible on some of our nearer planets, as Venus and Mars. In fact, that we can produce a distinct effect on one of these planets in this novel manner, namely, by disturbing the electrical condition of the earth, is beyond
any doubt.
"We are whirling through endless space with an inconceivable speed, all around us everything is spinning, everything is moving, everywhere is energy. There must be some way of availing ourselves of this energy more directly. Then, with the light obtained from the medium, with the power derived from it, with every form of energy obtained without effort, from the store forever inexhaustible, humanity will advance with giant strides. The mere contemplation of these magnificent possibilities expands our minds, strengthens our hopes and fills our hearts with supreme delight."
Nikola Tesla – 1895
TESLA was an electrical genius whose scientific discoveries and inventions were basic to modern electrical and electronic engineering. He also discovered and demonstrated the principles of high frequency, high potential currents shown in the historic photograph on the preceding page. These were the famous Colorado Springs experiments. The electromagnetic fields created were so intense that they perceptibly affected the distribution of the electrical potential of the earth. In Tesla's words, "In these experiments, effects were developed incomparably greater than any ever produced by human agencies, and yet these results are but an embryo of what is to be."
Such a force field can be applied widely, including electric aerospace propulsion. Within the next ten years electric propulsion will play a leading role in making extensive space trips possible. This conclusion has been ex- pressed in recent years by many researchers. They have compared the advantages and limitations of various space propulsion methods.
Chemical propulsion is the only presently available means for attainment of orbital speeds and altitudes. This is its chief value. Multimillion pound chemical super- boosters can put significant payloads into interplanetary orbits for manned expeditions to the moon, and possibly Venus and Mars. The estimated cost of these projects is staggering. In addition, the exploration of our nearest planets requires transit times of one to three years for a round trip planned on the capability of chemical propulsion. This aspect alone is sufficient to make electric propulsion a highly advantageous method of fuel conservation. For trips beyond Mars, electric propulsion is mandatory both to conserve fuel and also to shorten transit time. Chemical systems would require years or even decades for a round trip. Electrically propelled space vehicles have great payload capability. A Martian round trip, for example, has a payload ratio of almost 50 per cent. This means that these electric vehicles will offer comfortable living space for "shirt-sleeve" environment and adequate power for utilities.
Most electric propulsion systems are very small thrust devices. This limits them to missions beyond the atmosphere of the earth. Because of this, it is believed that this shortcoming is in the nature of electric propulsion. Consequently, it appears that orbit injection can only be accomplished by chemical means, and by chemo-nuclear means in the future. Once the orbit is established, the electric system would take over in providing thrust.
There are very severe problems in maneuvering spacecraft. For example, the spacecraft may require a radically changing course, should an unexpected emergency occur during any point of trajectory.
Such maneuverability is absolutely necessary for practical space systems of the future which have progressed beyond the development stage of present rockets. Both the injection into orbit and practical maneuverability in space demand high thrust propulsion and fuel economy simultaneously. A possibility of meeting these requirements is electro-chemical propulsion. Here, chemical fuels provide a slight exhaust mass which is accelerated by ultra high electromagnetic fields. The prime source of vehicle energy, capable of producing the extremely high force fields, must not require chemical fuels for its own operation. This requires nuclear energy sources or some practical system of converting radiation energy pervading space. In either case, the vehicle size is certain to be large to accommodate the primary energy source. Its weight must not exceed a reasonable fraction of the vehicle's gross weight. Spaciousness is required for physiological and psychological comfort of the crew as well as to increase the safety against meteorite hazards by an interlock escape system. Most approaches involve the study of assembling large structures in space by combining rendezvous techniques with payload capability of large chemical boosters. However, there are severe problems of weightlessness, inertial forces of large parts floating in space, gyroscopic and tidal forces warping large space structures in various stages of assembly, and hazards to men working in free space.
An alternative to this approach of assembling large vehicles in space is being investigated at Ryan as a part of an Electric Aerospace Propulsion concept based on the following:
A completely assembled, large aerospace vehicle should be capable of performing throughout the altitude range, from hovering at sea level to the attainment of orbital speeds, in such a manner as to include the performance characteristics of a helicopter, a propeller aircraft, a jet airplane, a ramjet and a space vehicle into an integrated system design.
Theoretical investigations based on this premise and supported by an initial experimental program have indicated a possible solution to this objective. The key is contained in the afore- mentioned concept of electro-chemical propulsion, enlarged by the concept of an electric air breathing engine. Efficiency requires that the velocity of the exhaust jet should be matched to the vehicle velocity. At low speeds the jet velocity should be small. As vehicle speed is increased, so also should the jet velocity be increased to maintain high efficiency of energy conversion. However, using small jet velocities for take-off requires a large exhaust mass, as in the case of a helicopter whose rotor causes a large air mass to move with relatively small downwash velocity. At the somewhat higher speeds developed by subsonic aircraft, the rotor of a helicopter is replaced by a propeller which moves a smaller air mass at higher speeds. At the supersonic velocities of a jet airplane, the flow of exhaust mass is still smaller but its velocity is further increased.
With an electric air breathing engine this can be achieved by force field control, capable of moving large air masses at low speeds and smaller air masses at higher velocities. A number of vehicle geometries are suitable for satisfying the requirement of velocity and mass control of the exhaust jet. One such geometry, offering additional design advantages of minimum structural weight, large volume and cargo capacity combined with desirable aerothermodynamic characteristics, is shown in the illustration as a circular disk vehicle. This geometry is also particularly suitable for hovering close to ground, because the annular jet augments very substantially the cushion effect of the air trapped between the vehicle and the ground.
By these principles, the efficiency and the thrust of electric aerospace propulsion can be maintained at high levels throughout the entire velocity and altitude range. After leaving the atmosphere, electric propulsion consists of a combination of intense force fields accelerating colloidal chemical plasma; the heavier elements being
used for high thrust performance and lighter elements for sustained vehicle acceleration.
Research is continuing in the area of generation and control of high electro- magnetic field intensities and colloidal plasma combined with the principle of an electric air breathing engine. Aeroelectric propulsion is expected to be a practicable and valuable method for powering aerospace vehicles.”
At/from the wonderful Internet Archive website:
ia800700.us.archive.org/2/items/ryanreporter231263ryan/ry...
Very nice artwork by Ryan Aeronautical staff artist Matt Giacalone.
Company/Owner: HM Transport, Inc.
Fleet/Bus Number: A-8058
Classification: Air-conditioned Provincial Bus
Coachbuilder: Autodelta Coach Builders, Inc.
Body Model: Volvo/Autodelta B7R Coach (GL6127HKC2) (in Volvo 9800 front fascia)
Engine Model: Volvo D7E-290 (D7E11)
Chassis Model: Volvo B7R (YV3R6R62*GA)
Transmission: 6-speed Automatic Transmission
Suspension: Air Suspension
Seating Configuration: 2×2
Seating Capacity: 49
Franchise route: Santa Cruz (Laguna)–Cubao (Quezon City) via Los Baños
Route: Santa Cruz, Laguna–Cubao, Quezon City via N66 (Calamba–Pagsanjan Road) / E2 (SLEX-Turbina–SLEX-Magallanes)
Municipalities/cities passing: Pila/Victoria/Calauan/Bay/Los Baños/Calamba City–Magallanes (Makati City)
Type of Operation: Provincial Operation Public Utility Bus (Regular Class)
Area of Operation: CALABARZON (Region IV-A)
Shot Location: EDSA-Boni, Mandaluyong City
Date Taken: May 14, 2018
Notices:
* Please DON'T GRAB A PHOTO WITHOUT A PERMISSION. If you're going to GRAB IT, please give A CREDIT TO THE OWNER. Also, don't PRINT SCREEN my photos.
** If I have mistakes on the specifications, please comment in a good manner so that I can edit it immediately.
*** The specifications and routes (for provincial, inter-provincial, and city operation) mentioned above are subjected for verification and may be changed without prior notice.
**** The vehicle's registration plate(s), conduction sticker(s), and/or persons (if applicable) were pixelated/blurred to prevent any conflict with the photographer, the bus company and/or to the car owner for their security and/or privacy purposes. So, don't use their plate number, conduction sticker, and vehicle tag as an evidence for any incident. And, I have taken this photo for bus fanatics, bus enthusiasts, and bus lovers purposes.
The best fit configuration ever for me.
- The new Compass Randonneur 42cm handlebars on a 5cm Nitto stem have finally given me the right fit for drop bars with no pain on my hands or neck.
- The Nitto lugged seat post with its extended setback has allowed me to position the saddle right where I want it, which the standard Nitto seat post didn't allow.
- The Brooks C17 is the most comfortable saddle I've ever tried on a road bike. It's now on all my bikes. Couldn't quite find the same experience with the leather saddles.
- The 35mm Compass Bon Jon Pass are a world of difference better and smoother than the 35 Schwalbe Marathon tires and even the 32 Cypress Legers I had after the Marathons.
NTI and JJV Transport
Truck
MAN Truck Shell Oil Company
Model: MAN TGS 26.360
Chassis: 26.360
Axle Configuration: 6x4
Trailer : 3 Axle Shell Tanker Transbuilt Trailer
Shot Location: Batangas City
How I finally made it comfortable...
- Nitto Grand Bois Elysées handlebar for a nice upright position that still allows me to lean forward due to the 11cm Nitto Tallux stem. Brooks Cambium natural tape to match the saddle.
- Brooks Cambium Carved saddle in natural. Very comfortable and allows about an extra inch of rear saddle positioning which for me, was what I needed to relieve hand pressure and be more comfortable.
Other stuff that made a huge difference:
- Compass Barlow Pass 38mm tires - huge difference in ride comfort and suppleness compared to the previous Schwalbe Marathon Racers I had before.
I'll be installing the fenders next week.
Victory Liner Inc.
Bus number: 8037
Classification: Airconditioned Provincial Operation Bus
Coachbuilder: Hyundai Motor Company
Chassis: KMJTA18VPAC
Model: Hyundai Aero City - First Generation
Engine: Hyundai D6AV
Layout: Rear-Mounted Engine Rear-Wheel Drive
Airconditioning Unit: Overhead Unit
Suspension: Leaf Spring Suspension
Seating Configuration: 3x2
Seating Capacity: 56 Passengers
Shot Location: Victory Liner Caloocan Terminal