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The Aerojet Rocketdyne RS-25, otherwise known as the Space Shuttle main engine (SSME), is a liquid-fuel cryogenic rocket engine that was used on NASA's Space Shuttle and is planned to be used on its successor, the Space Launch System. Built in the United States by Rocketdyne, the RS-25 burns cryogenic liquid hydrogen and liquid oxygen propellants, with each engine producing 1,859 kN (418,000 lbf) of thrust at liftoff. Although the RS-25 can trace its heritage back to the 1960s, concerted development of the engine began in the 1970s, with the first flight, STS-1, occurring on April 12, 1981. The RS-25 has undergone several upgrades over its operational history to improve the engine's reliability, safety, and maintenance load.
The engine produces a specific impulse (Isp) of 452 seconds (4.43 km/s) in a vacuum, or 366 seconds (3.59 km/s) at sea level, has a mass of approximately 3.5 tonnes (7,700 pounds), and is capable of throttling between 67% and 109% of its rated power level in one-percent increments. The RS-25 operates at temperatures ranging from −253 °C (−423 °F) to 3300 °C (6000 °F).
The Space Shuttle used a cluster of three RS-25 engines mounted in the aft structure of the orbiter, with fuel being drawn from the external tank. The engines were used for propulsion during the entirety of the spacecraft's ascent, with additional thrust being provided by two solid rocket boosters and the orbiter's two AJ10-190 orbital maneuvering system engines. Following each flight, the engines were removed from the orbiter, inspected, and refurbished before being reused on another mission. Source: Wikipedia
© 2017 Skip Plitt Photography, All Rights Reserved.
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Todos los derechos reservados. Esta foto no se puede utilizar en cualquier forma sin el permiso del fotógrafo.
A truly amazing inboard profile/cutaway view of a complete space shuttle stack, ca. 1983.
An earlier version, understandably less precise, detailed or refined, prior to the flight of STS-1, can be seen at the following:
www.youtube.com/watch?v=XuldqDPk3mE
Credit: AIRBOYD/YouTube (AIRBOYD having many excellent videos of a variety of aerospace/rocketry footage btw)
The gracious generosity of Angela Carole Brown revealed this - in my estimation – masterpiece, to be by the hand of her father, Ted Brown, as I’m sure the precursor is as well.
Commencing at the 1:33 mark. A beautiful & touching remembrance/memorial:
www.youtube.com/watch?v=D-w4MHqTx5A
Credit: Angela Carole Brown/YouTube
Click on the “Ted Brown” tag & prepare to be blown away.
The only other place it appears to be available is one of the pay-to-play sites, which I won't dignify with its link.
Circa 1974 Rockwell International artist’s concept depicting an orbit insertion/circularization burn of the Space Shuttle’s Orbital Maneuvering System (OMS) engines.
Occasionally/more ‘commonly’ seen as a lithograph. Of course, I can’t find an example in order to provide a Rockwell ‘party line’ caption.
Beautiful artwork by Rockwell International artist supreme, Manuel E. Alvarez.
A mocking/taunting 月亮 can be seen, still out of reach, in the distantly distant distance.
A cropped version of the image, with subtle differences in the markings on the spacecraft, is featured on the cover of the 1988 book “SPACE SHUTTLE”, written by David Baker.
Speaking of out of reach, the U.S. is firmly in the process of losing the “high-ground”…if it hasn’t lost it already:
www.getrevue.co/profile/aj_fi/issues/china-space-news-upd...
And check this out, this enterprising SOB has gone apeshit with a bunch of photos I’ve posted and/or linked to in my postings:
www.redbubble.com/i/photographic-print/Space-Shuttle-s-Or...
“Artist’s concept shows protective shroud falling away, exposing eight communications satellites in their dispenser on board the transtage of the Air Force’s Titan III-C booster. The transtage will place the satellites in an 18,200 nautical mile near-synchronous, equatorial orbit. The multiple launch technique -- provides an economical means of establishing a military communication satellite system.”
Artist unknown, although the stylistic last two letters of "nt" are visible at the left edge of the image.
Expected waviness along the top edge due to the copious everlasting military grade adhesive used to affix the description.
Also:
www.drewexmachina.com/2015/06/18/the-first-missions-of-th...
Credit: Andrew LePage/DREW Ex Machina website
space.skyrocket.de/doc_sdat/idcsp.htm
Credit: "GUNTER'S SPACE PAGE" website
en.wikipedia.org/wiki/Initial_Defense_Communications_Sate...
Credit: Wikipedia
Despite the apparent multiple-choice nature of the affixed caption, based on the 8/17/92 date on the caption & loosely, on other sort of similarly numbered photos – I’m going with “b”/“no. 2”.
Obviously, meant for internal consumption, so I’ll cut the NASA photo ‘professionals’ some undeserved slack.
So, I’m going to assume the following applies, regardless of choice:
“VAB/OMEF OPERATIONS.”
With that, my final answer, at least for now, is:
“STS-47. OV-105. BEFORE MATED TO STACK.”
Finally, “CUSTOMER EXPOSED FILM-D’ARCANGELO” means…what? Mr./Ms. D’Arcangelo? Was he/she the photographer? If so, representing/working for/contracted by…the “customer”? Rockwell Int'l/Rocketdyne maybe, based on the “VAB/OMEF” nomenclature in the caption? BTW, there’s very little available on the OMEF, which I’m guessing was located within the VAB & possible predecessor to the Space Shuttle Main Engine Processing Facility (SSMEPF), which appears to have been located within/adjacent(?) to OPF-3. Whatever…close enough.
All that really matters is that it’s a damned good photograph of space flight stuff.
I've forgotten why, but I think these photographs support my identification:
georgesrockets.com/GRP/Scale/ShuttleData/HTMLshuttlepics/...
Credit: George Gassaway's wonderful site, "George's Rocketry Pages" website. No longer maintained, it will mark another sad day when it is no longer available, which I'm sure is sooner rather than later.
A beautiful artist’s concept of an earth-orbiting Apollo Applications Program (AAP) configuration, possibly of an experimental micro-gravity biology module…maybe… ¯\_(ツ)_/¯…docked to the Apollo Command/Service Module (CSM).
The scientist-astronaut seems – I think – to be using a snazzy microscope of some sort, although I’m having some perspective issues regarding it, to include what the large rectangular component with the conical appendage is being used for. Photomicrography? And how it correlates with the other components in the immediate vicinity, which may include dual/binocular eyepieces?
Note also the item that looks like a bubble helmet on the half shelf to the left of the scientist-astronaut. I think I see the vague, barely perceptible features of a human head inside it. Do you see it??? GOOD GOD, what kind of unholy experiments were under consideration?!? 😲😉
And, I can’t seem to identify the rough, textured, metallic(?)…’mass’ depicted on the other side of the module, across from the scientist-astronaut. And, it looks like there’s a fixed stool in front of it.
Based on the strong similarity of this CSM to that in another work I’ve linked to below, which is also from this series of works (based on photo ID no. sequence), I really think it, and this one is by Raymond Bruneau. That other one has the letters “RB”, with an arrow adjacent to it, depicted as if it were part of the surface markings on the exterior of the Service Module. That, and the fact that Mr. Bruneau chose to use actual photographs of the earth in a number of his earth orbit depictions, such as this one, gives me confidence in my identification.
Finally, although I haven’t been able to find a match from the exemplars available online, I’m sure the Neil Armstrong signature is an autopen.
AJ10 BUS is a Dennis Javelin/Plaxton Panther C57F, new to Andybus, Dauntsey, Wiltshire in March 2010.
This Volvo XC70 from the UK, was travelling along the A1 autobahn. The car was registered in May 2010, originally registered to the town of Peterborough, located in east-central England.
A1 Autobahn (Stuhr), Lower Saxony, Germany
I have been trying to acquire this Apollo CSM engine for many years now. Norton Sales has held onto it for the past 50 years. They received it in 1970 from Rocketdyne after returning the gold bricks they accidentally found in a surplus sales lot. This SPS engine will seen in the forthcoming third season of For All Mankind . Specifically, a Block I AJ10-137 engine from 1964.
And the 48" diameter titanium fuel tanks, also from the CSM, were in a Transformers movie. That RASCAL engine on the right comes from the first nuclear-tipped supersonic air to surface missile, from the 1950's. The sleigh also included other Apollo engine artifacts like a J-2 impeller and part of a F-1 gas generator.
Santa must think I have been a very good boy! And who knew? Xmas in July a thing!
This Service Propulsion System (SPS) Engine was constructed by Aerojet General Corporation out of Sacramento, California for the Apollo Lunar Program. It was the first man-rated propulsion system to be certified to take humans beyond earth orbit.
After separating from the Saturn V S-IVB, the SPS engine provided the thrust for all major CSM spacecraft velocity changes throughout an Apollo mission. The engine has a nominal 20,500 pound thrust and could be fired for a minimum of 0.4 seconds. Its design required that it successfully fired every time on command, or the Apollo Crew would never return home safely after a lunar landing.
Here are the specs, and a video overview (PSWD Carlos):
MOD AJ10-137 APOLLO ENGINE
NAA/S&ID control:
Part no. ME 901-0007-0003
Contract No. M3J7XA-406014
MFD Date. 4-0-64
MFR Serial No. 001890000022
MFR Part No. 707170-15
The heroic engine that brought Apollo back from the moon, well except for Apollo 13. Assembled and tested in Q2, 1969.
With only one combustion chamber and expansion nozzle in space, engineers designed a simple SPS 20,500-pound thrust engine to perform flawlessly each time. Instead of mechanical pumps with moving parts, helium forced fuel and oxidizer into the combustion chamber. With no throttle, the engine either burned wide open or was off. To simplify the ignition system, the SPS engine’s fuel and oxidizer ignited on contact with each other (hypergolic fuels requiring no igntion system).
The SPS engine was the Aerojet AJ10-137, which used Aerozine 50 as fuel and nitrogen tetroxide (N2O4) as oxidizer to produce 20,500 lbf (91 kN) of thrust.
An artifact in the Future Ventures’ 🚀 Space Collection.
“Aerojet-General Corporation artist’s concept shows how the Apollo spacecraft’s Service Module engine will look firing during night flight. Coloration of the Service Propulsion System thrust chamber and skirt shows temperature ranging from 5000°F. at the chamber throat to 1200°F. at the skirt extension after a few seconds of engine operation. Glass filament is used in the thrust chamber area. The engine skirt is formed of titanium and columbium. Aerojet’s SPS develops in excess of 20,000 pounds of thrust, making it America’s largest and most powerful spacecraft rocket engine. The Service Propulsion System, produced for NASA’s Apollo spacecraft under contract to North American Rockwell Space Division, is capable of providing more than 35 separate firings of varying duration.”
~7.5” x ~9.25”. Photo has been trimmed by some well-intentioned buffoon in the past.
Compare/contrast. Note that the respective glowing (hotter?) areas of the two engine nozzles are inverted. I would’ve expected them to be somewhat similar. Interesting:
mobile.twitter.com/SpaceX/status/1076838618692493313/photo/1
Credit: SpaceX
Check this one out. No idea what the engine is and obviously not in flight, yet another totally different appearance:
qph.c7.quoracdn.net/main-qimg-099ffe22085d444e4d61a6c61a9...
Credit: Quora website
The artist appears to have used the Impasto painting technique for the overall scene, with the CSM & SPS plume painted “normally”.
I think this is the work of George Mathis.
UK10 ECS (ex VU10 XNB, AJ10 BUS)
2010 Alexander Dennis Javelin/Plaxton Profile C55F
Ebley Coach Services, Nailsworth, Gloucestershire
Buckingham, 12 March 2025
New to Andybus, Dauntsey
“Aerojet-General Corporation artist’s concept shows how the Apollo spacecraft’s Service Module engine will look firing during night flight. Coloration of the Service Propulsion System thrust chamber and skirt shows temperature ranging from 5000°F. at the chamber throat to 1200°F. at the skirt extension after a few seconds of engine operation. Glass filament is used in the thrust chamber area. The engine skirt is formed of titanium and columbium. Aerojet’s SPS develops in excess of 20,000 pounds of thrust, making it America’s largest and most powerful spacecraft rocket engine. The Service Propulsion System, produced for NASA’s Apollo spacecraft under contract to North American Rockwell Space Division, is capable of providing more than 35 separate firings of varying duration.”
8.5" x 11".
Compare/contrast. Interesting that the respective glowing areas of the two engines are inverted:
mobile.twitter.com/SpaceX/status/1076838618692493313/photo/1
Credit: SpaceX
Check this one out. No idea what the engine is and obviously not in flight, yet another totally different appearance:
qph.c7.quoracdn.net/main-qimg-099ffe22085d444e4d61a6c61a9...
Credit: Quora website
Despite its appearance, the photograph has not been folded, spindled or mutilated. The artist appears to have used the Impasto painting technique for the overall scene, with the CSM & SPS plume painted “normally”.
I think this is the work of George Mathis.
"This view of the space shuttle Columbia (STS-2) was made with a hand-held 70mm camera in the rear station of the T-38 chase plane. Mission Specialist/Astronaut Kathryn D. Sullivan exposed the frame as astronauts Joe N. Engle and Richard H. Truly aboard the Columbia guided the vehicle to an unpowered but smooth landing on the desert area of Edwards Air Force base in California. The view provides a good study of the high temperature protection material on the underside of the spacecraft which is exposed to the friction on the atmospheric entry on the return to Earth. Also note trails from the wing tips." And that the rudder/speed brake is partially open.
Above applicable description taken from that for photo S81-39563, the near equivalent photo:
images.nasa.gov/details-S81-39563.html
Also:
earthobservatory.nasa.gov/Features/ShuttleRetrospective/i...
Credit: NASA 'Earth Observatory' website
Photo from Art Lebrun Flickr / REMASTERED by Dan Beaumont.
INFO: The Vanguard rocket[1] was intended to be the first launch vehicle the United States would use to place a satellite into orbit. Instead, the Sputnik crisis caused by the surprise launch of Sputnik 1 led the U.S., after the failure of Vanguard TV3, to quickly orbit the Explorer 1 satellite using a Juno I rocket, making Vanguard I the second successful U.S. orbital launch.
Vanguard rockets were used by Project Vanguard from 1957 to 1959. Of the eleven Vanguard rockets which the project attempted to launch, three successfully placed satellites into orbit.
In 1955, the USA announced plans to put a scientific satellite in orbit for the International Geophysical Year (IGY) in 1957-1958. The goal was to track the satellite as it performed experiments. At that time there were three candidates for the launch vehicle: The Air Force's SM-65 Atlas, a derivative of the Army Ballistic Missile Agency's SSM-A-14 Redstone, and a Navy proposal for a three-stage rocket based on the RTV-N-12a Viking sounding rocket.[2]
The Army's Redstone-based proposal would likely be first ready for a first satellite launch. Its connection with German-born scientist Wernher von Braun, however, was a public relations risk.[2] In any case, the Atlas and Redstone ballistic missiles were top-priority military projects, which were not to be slowed by pursuing a secondary space launch mission. Vanguard was a project of the Naval Research Laboratory (NRL), which was regarded more as a scientific than a military organization. This helped to emphasize the non-military goals of the satellite program. This was considered important, because a discussion of whether overflights of foreign countries by satellites were legal or illegal was to be avoided.
In August or September 1955, the DOD Committee on Special Capabilities chose the NRL proposal, named Vanguard, for the IGY project. The Martin company, which had also built the Viking, became prime contractor for the launch vehicle.[3] The Vanguard rocket was designed as a three-stage vehicle. The first stage was a General Electric X-405 liquid-fueled engine (designated XLR50-GE-2 by the Navy), derived from the engine of the RTV-N-12a Viking. The second stage was the Aerojet General AJ10-37 (XLR52-AJ-2) liquid-fueled engine, a variant of the engine in the RTV-N-10 Aerobee. Finally, the third stage was a solid-propellant rocket motor. All three-stage Vanguard flights except the last one used a motor built by the Grand Central Rocket Company. Vanguard had no fins, and the first and second stages were steered by gimbaled engines. The second stage also housed the vehicle's telemetry system, the inertial guidance system and the autopilot. The third stage was spin stabilized, the spin being imparted by a turntable on the second stage before separation.
Launch summary[edit]
The first two flights of the Vanguard program, designated Test Vehicle (TV)-0 and -1, were actually the last two remaining RTV-N-12a Viking rockets. TV-0, launched on December 8, 1956, primarily tested new telemetry systems, while TV-1 on May 1, 1957 was a two-stage vehicle testing separation and ignition of the solid-fueled upper stage of Vanguard. TV-2, launched on October 23, 1957 after several abortive attempts, was the first real Vanguard rocket. The second and third stages were inert, but the flight successfully tested first/second-stage separation and spin-up of the third stage. However, by that time, the Soviet Union had already placed the "Sputnik" satellite into orbit, and therefore project Vanguard was more or less forced to launch its own satellite as soon as possible. Therefore, a very small experimental satellite (called the "grapefruit" and weighing only 1.8 kg (4 lb)) was added to TV-3, which was to be the first test of an all-up Vanguard rocket. Although the NRL and Martin tried to emphasize that the TV-3 mission was a pure test flight (and one with several "firsts"), everyone else saw it as the first satellite launch of the Western world, billed as "America's answer to Sputnik". Wernher von Braun angrily said about the Sputnik launch: "We knew they were going to do it. Vanguard will never make it. We have the hardware on the shelf. We can put up a satellite in 60 days".[4]
On 6 December the US Navy launched a Vanguard rocket, carrying a 1.3 kg (2.9 lbs) satellite, from Cape Canaveral. It only reached an altitude of 1.2 meters (4 ft), fell and exploded. The satellite was blasted off the top of the rocket where it landed in bushes near the pad and began transmitting signals, leading to New York Journal-American columnist Dorothy Kilgallen remarking "Why doesn't somebody go out there, find it, and shoot it?" The American press called it Kaputnik.[5]
File:1958-02-06 Vanguard Fails in Second Launching.ogv
Newsreel of Vanguard TV3 Backup launch
Flight TV-3BU (BU = Backup) on February 5, 1958 broke up after 57 seconds because of a control system malfunction, but TV-4 on March 17, 1958 finally succeeded in placing a "Grapefruit"-type satellite into orbit. By that time, however, the Army's Juno (Jupiter-C) had already launched the United States' first satellite. The TV-4 satellite, labeled Vanguard 1, reached a relatively high orbit (3966 km (2465 miles) x 653 km (406 mi)) and is currently the oldest human artifact in space. The following four flights, TV-5 and SLV (Satellite Launch Vehicle)-1 through -3 all failed, but on February 17, 1959, SLV-4 launched Vanguard 2 (weighing 10.8 kg (23.7 lb)) into orbit. The SLVs were the "production" Vanguard rockets. SLV-5 and -6 also failed, but the final flight on September 18, 1959 successfully orbited the 23.6 kg (52 lb) Vanguard 3 satellite. That last mission was designated TV-4BU, because it used a remaining test vehicle, which had been upgraded with a new third stage, the Allegheny Ballistics Lab X-248A2 Altair. This more powerful motor enabled the launch of the heavier payload. The combination of the AJ10 liquid engine and X-248 solid motor was also used, under the name Able, as an upper stage combination for Thor and Atlas space launch vehicles.
Launches[edit]
Vanguard launched 3 satellites out of 11 launch attempts:
Vanguard TV3 - December 6, 1957 - Failed to orbit 1.36 kg (3 lb) satellite
Vanguard TV3 Backup - February 5, 1958 - Failed to orbit 1.36 kg (3 lb) satellite
Vanguard 1 - March 17, 1958 - Orbited 1.47 kg (3.25 lb) satellite
Vanguard TV5 - April 28, 1958 - Failed to orbit 10.0 kg (22 lb) satellite
Vanguard SLV 1 - May 27, 1958 - Failed to orbit 10.0 kg (22 lb) satellite
Vanguard SLV 2 - June 26, 1958 - Failed to orbit 10.0 kg (22 lb) satellite
Vanguard SLV 3 - September 26, 1958 - Failed to orbit 10.0 kg (22 lb) satellite
Vanguard 2 - February 17, 1959 - Orbited 9.8 kg (21.6 lb) satellite
Vanguard SLV 5 - April 13, 1959 - Failed to orbit 10.3 kg (22.7 lb) satellite
Vanguard SLV 6 - June 22, 1959 - Failed to orbit 10.3 kg (22.7 lb) satellite
Vanguard 3 - September 18, 1959 - Orbited 22.7 kg (50 lb) satellite[6]
Unsuccessful launch of Vanguard TV-3 at Cape Canaveral (December 6, 1957).
Vanguard US satellite program, Vanguard: A Rocket For Science movie, 1958 VIDEO: www.youtube.com/watch?v=l16QZJLQHwg
VANGUARD LAUNCH, TV-4, March 17 1958 VIDEO:
“AEROJET APOLLO MOON ROCKET -- Apollo astronauts depend on this rocket engine built by Aerojet-General Corporation to provide the pushing power to make major course changes for the Apollo spacecraft during earth orbital and lunar missions. It is the Service Propulsion System rocket engine which produces 20,500 pounds of thrust and stands 13 feet four inches tall.”
In color; however, disparate photo numbers suggest it being another engine::
2.bp.blogspot.com/-Sz9rFfKdvwk/Viz_rvRXhkI/AAAAAAAAC9U/l0...
Credit: The excellent Exo Cruiser website
See also:
airandspace.si.edu/collection-objects/rocket-engine-liqui...
SCAN AND REMASTERED by Dan Beaumont. (Vanguard Navy Space Program) WIKIPEDIA INFO: The first two flights of the Vanguard program, designated Test Vehicle (TV)-0 and -1, were actually the last two remaining RTV-N-12a Viking rockets. TV-0, launched on December 8, 1956, primarily tested new telemetry systems, while TV-1 on May 1, 1957 was a two-stage vehicle testing separation and ignition of the solid-fueled upper stage of Vanguard. TV-2, launched on October 23, 1957 after several abortive attempts, was the first real Vanguard rocket. The second and third stages were inert, but the flight successfully tested first/second-stage separation and spin-up of the third stage. However, by that time, the Soviet Union had already placed the "Sputnik" satellite into orbit, and therefore project Vanguard was more or less forced to launch its own satellite as soon as possible. Therefore, a very small experimental satellite (called the "grapefruit" and weighing only 1.8 kg (4 lb)) was added to TV-3, which was to be the first test of an all-up Vanguard rocket. Although the NRL and Martin tried to emphasize that the TV-3 mission was a pure test flight (and one with several "firsts"), everyone else saw it as the first satellite launch of the Western world. Wernher von Braun angrily said about the Sputnik launch: "We knew they were going to do it. Vanguard will never make it. We have the hardware on the shelf. We can put up a satellite in 60 days".[4]
On 6 December the US Navy launched a Vanguard rocket, carrying a 1.3 kg (2.9 lbs) satellite, from Cape Canaveral. It only reached an altitude of 1.2 meters (4 ft), fell and exploded. The satellite was blasted off the top of the rocket where it landed in bushes near the pad and began transmitting signals, leading to New York Journal-American columnist Dorothy Kilgallen remarking "Why doesn't somebody go out there, find it, and shoot it?" The American press called it Kaputnik.[5]
File:1958-02-06 Vanguard Fails in Second Launching.ogv
Newsreel of Vanguard TV3 Backup launch
Flight TV-3BU (BU = Backup) on February 5, 1958 broke up after 57 seconds because of a control system malfunction, but TV-4 on March 17, 1958 finally succeeded in placing a "Grapefruit"-type satellite into orbit. By that time, however, the Army's Juno (Jupiter-C) had already launched the United States' first satellite. The TV-4 satellite, labeled Vanguard 1, reached a relatively high orbit (3966 km (2465 miles) x 653 km (406 mi)) and is currently the oldest human artifact in space. The following four flights, TV-5 and SLV (Satellite Launch Vehicle)-1 through -3 all failed, but on February 17, 1959, SLV-4 launched Vanguard 2 (weighing 10.8 kg (23.7 lb)) into orbit. The SLVs were the "production" Vanguard rockets. SLV-5 and -6 also failed, but the final flight on September 18, 1959 successfully orbited the 23.6 kg (52 lb) Vanguard 3 satellite. That last mission was designated TV-4BU, because it used a remaining test vehicle, which had been upgraded with a new third stage, the Allegheny Ballistics Lab X-248A2 Altair. This more powerful motor enabled the launch of the heavier payload. The combination of the AJ10 liquid engine and X-248 solid motor was also used, under the name Able, as an upper stage combination for Thor and Atlas space launch vehicles.
AJ10 BUS
Plaxton Panther / Dennis Javelin
Andrew James Travel of Malmesbury
Location: Wellsway, Bath
Date: 03/12/2017
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AJ10 BUS is a Dennis Javelin/Plaxton Panther C57F, new to Andybus, Dauntsey, Wiltshire in March 2010.
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Copyright © P.J. Cook, all rights reserved. It is an offence to copy, use or post this image anywhere else without my permission.
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AJ10 BUS is a Dennis Javelin/Plaxton Panther C57F, new to Andybus, Dauntsey, Wiltshire in March 2010.
Want to find out more? Join The PSV Circle - Details at www.psvcircle.org.uk
Copyright © P.J. Cook, all rights reserved. It is an offence to copy, use or post this image anywhere else without my permission.
AJ10 TOW : Land Rover Defender 110 'Workshop' Hard Top of
A J Autos Recovery from Weston-super-Mare, Somerset.
TRUCKFEST SOUTH-WEST 2024
Bath & West Showground, Shepton Mallett.
31-08-2024
An orbital maneuvering system (OMS) engine firing caused this bright glow at the aft end of the shuttle Challenger during the STS-7 mission. Also visible in the open payload bay are parts of the Shuttle pallet satellite, the experiment package for NASA's Office of Space and Terrestrial Applications, the protective cradles for the Indonesian Palapa-B and Telesat Canada Anik C2 satellites, some getaway special canisters and the Canadian-built remote manipulator system. Only a small portion of the earth's horizon can be seen above the orbiter's vertical stabilizer.
25 June 1983
KENNEDY SPACE CENTER, FLA. The Boeing Delta II Heavy second-stage engine, the Aerojet AJ10-118K, is lifted up the mobile service tower at Pad 17-B, Cape Canaveral Air Force Station. The Delta II is the launch vehicle for the MESSENGER (Mercury Surface, Space Environment, Geochemistry and Ranging) spacecraft, scheduled to lift off Aug. 2. Bound for Mercury, the spacecraft is expected to reach orbit around the planet in March 2011. MESSENGER was built for NASA by the Johns Hopkins University Applied Physics Laboratory in Laurel, Md. Image from NASA, originally appeared on this site: science.ksc.nasa.gov/gallery/photos/ Reposted by San Diego Air and Space Museum