The AJ10 is a hypergolic rocket engine manufactured by Aerojet Rocketdyne (previously Aerojet). It has been used to propel the upper stages of several...

the XASR-1 (21AL-2600), 45AL-2600, AJ10-24, AJ10-25, AJ10-27, AJ10-34, AJ11-6, and AJ60-92. Later versions of the AJ10 and AJ-11 engines produced 17.8 kilonewtons...

vehicles. The AJ10 engine which made up those stages was adapted into the AJ10-137, which was used as the Apollo Service Module engine. The AJ10-190, adapted...

stage of the Vanguard rocket, as the AJ10-118 configuration. It was initially fueled by nitric acid and UDMH. An AJ10 engine was first fired in flight during...

fuselage, on either side of the vertical stabilizer. Each pod contains a single AJ10-190 engine, based on the Apollo Service Module's Service Propulsion System...

and development of the stage took a mere eight months. A version of the AJ10 engine used for the Able rocket stage was used as the engine of Apollo Service...

thought to include the AJ10-118k; used for the second stage of the Delta II it is a lighter and more powerful version in the same AJ10 engine family whose...

II was the Delta-K, powered by a restartable (up to six restarts) Aerojet AJ10-118K engine burning hypergolic Aerozine-50 and N2O4. These propellants are...

AJ10 series, which includes the AJ10-37 engine on the second stage of the world's first purpose-built satellite launch vehicle, Vanguard. Other AJ10 series...

total thrust increased by two solid rocket boosters and the orbiter's two AJ10 orbital maneuvering system engines. Following each flight, the RS-25 engines...

purpose Satellite Launch Vehicle, Vanguard. The AJ10 engine used by many Aerobees eventually evolved into the AJ10-190 which formed the Orbital Maneuvering System...

the Moon in the direct ascent mission mode, The engine selected was the AJ10-137, which used Aerozine 50 as fuel and nitrogen tetroxide (N2O4) as oxidizer...

Maneuvering System (OMS) consisted of two aft-mounted AJ10-190 engines and the associated propellant tanks. The AJ10 engines used monomethylhydrazine (MMH) oxidized...

acid/UDMH, regeneratively cooled engine, was kept in place, but with an improved AJ10-118 engine. More significantly, the Delta stage featured cold gas attitude...

395 lb (4,715 kg) Max takeoff weight: 11,387 lb (5,165 kg) Powerplant: 2 × AJ10-138 rocket engine, 8,000 lbf (36 kN) thrust each Performance Maximum speed:...

the SLS, or even the Orion vehicle's own propulsion system (the Aerojet AJ10 engine) instead. The method of abort, either using the LAS or the second...

already record a panorama swing).[citation needed] October 5, 1954 Aerobee AJ10-24 RTV-N-10b The first color image from space as part in the left corner...

Aerojet 15NS-250 Aerojet 30AS-1000C – RATO unit Aerojet 2.2KS-11000 Aerojet AJ10 Aerojet AJ-260 – largest solid-rocket motor ever built Aerojet M-1 Aerojet...

interfaces modeled after those used in the Boeing 787 Dreamliner. It has a single AJ10 engine for primary propulsion, and others including reaction control system...

J J = from J10; denies higher honor 10 = from Q109, K109, A109, KJ10 or AJ10 9 = from 109; denies higher honor relatively high spot = discourages continuation...

launcher upper stages also use pressure-fed engines. These include the Aerojet AJ10 and TRW TR-201 used in the second stage of Delta II launch vehicle, and the...

rocket engine, 418,000 lbf (1,860 kN) thrust each Powerplant: 2 × Aerojet AJ10-190 liquid-fuelled rocket engine, 6,000 lbf (26.7 kN) thrust each Performance...

ramjet/scramjet engine flown on the Boeing X-51 hypersonic demonstration vehicle. AJ10 (Aerozine 50/N2O4) – Second stage engine for the Delta II, used as the Orbital...

rocket. Centaur (rocket stage) Inertial Upper Stage RM-81 Agena Wade, Mark. "AJ10-138". Encyclopedia Astronautica. Archived from the original on December 28...

December 16, 1999 Socorro LINEAR L4 36 km MPC · JPL 15528 Martinsmedina 2000 AJ10 Martinsmedina January 3, 2000 Socorro LINEAR FLO 2.3 km MPC · JPL 15529 2000...

began in the U.S. in March 2013. Toyota internally designated the iQ as the AJ10, with further sub-model chassis codes: The two seat variant was marketed...

January 10, 1998 Kleť J. Tichá, M. Tichý  · 6.3 km MPC · JPL 58683 1998 AJ10 — January 15, 1998 Caussols ODAS  · 2.5 km MPC · JPL 58684 1998 AA11 — January...

a Thor missile in the DM-21 configuration, and the second stage was the AJ10-118, which was derived from the earlier Delta-A. An Altair solid rocket motor...

acid/UDMH, regeneratively cooled engine, was kept in place, but with an improved AJ10-118 engine. More significantly, the Delta stage featured cold gas attitude...

October 1962 – Explorer 15 (EPE-C). The Delta B introduced the upgraded AJ10-118D upper stage, a three-foot propellant tank extension, higher-energy oxidizer...