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

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...

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...

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...

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...

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...

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...

interfaces modeled after those used in the Boeing 787 Dreamliner. A single AJ10 engine provides the spacecraft's primary propulsion, while eight R-4D-11...

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:...

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

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...

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...

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...

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...

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...

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...

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...

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...