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searching for Hypergolic propellant 18 found (102 total)

Larch (rocket engine) (56 words) [view diff] no match in snippet view article

The Larch was a family of rocket engine intended as an upgrade to Black Arrow launch vehicles. They were manufactured by Rolls-Royce between 1965 and 1971

R-4D (456 words) [view diff] no match in snippet view article find links to article

The R-4D is a small hypergolic rocket engine, originally designed by Marquardt Corporation for use as a reaction control system thruster on vehicles of

SpaceX Draco (855 words) [view diff] exact match in snippet view article find links to article

Dragon spacecraft. SuperDraco uses the same storable (non-cryogenic) hypergolic propellant as the small Draco thrusters, but is much larger and delivers over

Ascent propulsion system (733 words) [view diff] no match in snippet view article find links to article

The ascent propulsion system (APS) or lunar module ascent engine (LMAE) is a fixed-thrust hypergolic rocket engine developed by Bell Aerosystems for use

Dushkin S-155 (81 words) [view diff] no match in snippet view article find links to article

The Dushkin S-155 was a liquid-fueled rocket motor designed by Leonid Dushkin specifically for use in the Mikoyan-Gurevich Ye-50 and Ye-50A (aka MiG-23U)

S5.4 (375 words) [view diff] no match in snippet view article find links to article

The S5.4 (AKA TDU-1, GRAU Index 8D66), was a Russian liquid rocket engine burning TG-02 and AK20F in the gas generator cycle. It was originally used as

S5.142 (375 words) [view diff] no match in snippet view article find links to article

The S5.142 (AKA DST-25) is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85. It is used for crew-rated spacecraft propulsion applications

S400 (rocket engine) (257 words) [view diff] no match in snippet view article

The S400 is a family of pressure fed liquid propelled rocket engines manufactured by ArianeGroup (former Airbus DS) at the Orbital Propulsion Centre in

LEROS (457 words) [view diff] no match in snippet view article find links to article

LEROS is a family of chemical rocket engines manufactured by Nammo at Westcott, Buckinghamshire, United Kingdom. LEROS engines have been used as primary

BT-4 (rocket engine) (1,235 words) [view diff] no match in snippet view article

The BT-4 is a pressure-fed liquid rocket engine designed and manufactured by IHI Aerospace of Japan. It was originally developed for the LUNAR-A project

KTDU-35 (426 words) [view diff] no match in snippet view article find links to article

The KTDU-35 (GRAU Index 11D62) was a Soviet spacecraft propulsion system composed of two liquid rocket engines, the primary, S5.60 (SKD) and the secondary

11D428 (492 words) [view diff] no match in snippet view article find links to article

The 11D428A-16 (manufacturer's name RDMT-135M) is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85. It is used for crew-rated

S5.80 (639 words) [view diff] no match in snippet view article find links to article

The S5.80 is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85. It is used for crew-rated spacecraft propulsion applications. It

Société d'Etudes pour la Propulsion par Réaction (1,444 words) [view diff] no match in snippet view article find links to article

The Société d'Études pour la Propulsion par Réaction (SEPR) (in French: Jet Propulsion Research Company) was a French research and manufacturing company

KTDU-80 (2,808 words) [view diff] no match in snippet view article find links to article

The KTDU-80 (Russian: Корректирующе-Тормозная Двигательная Установка, КТДУ) is the latest of a family of integrated propulsion system that KB KhIMMASH

Research and Development Institute of Mechanical Engineering (826 words) [view diff] exact match in snippet view article find links to article

2.43 g (0.086 oz) per second of hypergolic propellant flow. CP2: 23.5 g (0.83 oz) per second of hypergolic propellant flow. CP3: 63 g (2.2 oz)/87 g (3

White Sands Test Facility (669 words) [view diff] exact match in snippet view article find links to article

private aerospace manufacturers is performed. WSTF refurbished hypergolic propellant components for the Space Shuttle, performed advanced pyrovalve testing

Chinese space program (20,639 words) [view diff] exact match in snippet view article find links to article

tetroxide and UDMH as propellant for liquid engines. Although this hypergolic propellant is simple, cheap and reliable, its disadvantages, including toxicity