RS-56
American kerolox rocket engine
RS-56 Country of origin United States First flight 1991 Manufacturer Rocketdyne Predecessor RS-27A Status Retired Propellant LOX / RP-1 Cycle Gas-generator Thrust, sea-level RS-56-OBA: 207,000 lbf (920.8 kN)RS-56-OSA: 60,500 lbf (269.0 kN)Chamber pressure 4.8 MPa (48 bar) Specific impulse , vacuumRS-56-OBA: 299 s (2.93 km/s)RS-56-OSA: 316 s (3.10 km/s)Specific impulse , sea-levelRS-56-OBA: 263 s (2.58 km/s)RS-56-OSA: 220 s (2.2 km/s)Burn time RS-56-OBA: 172RS-56-OSA: 283 secLength RS-56-OBA: 11.3 ft (3.43 m) 8.9 ft (2.7 m)Diameter RS-56-OBA: 8.0 ft (2.45 m) 10.0 ft (3.05 m)Atlas II
RS-56 (Rocket System-56) was an American liquid-fueled rocket engine, developed by Rocketdyne . RS-56 was derived from the RS-27 rocket engine,[ 1] which itself is derived from the Rocketdyne H-1 rocket engine used in the Saturn I and Saturn IB . Two variants of this engine were built, both for use on the Atlas II rocket series. The first, RS-56-OBA, was a booster engine, while the RS-56-OSA was designed for use as a sustainer and produced lower thrust but at a higher specific impulse .[ 2] [ 3]
References
Liquid fuel
Cryogenic
Hydrolox (LH2 / LOX )
China
Europe
India
Japan
Russia
United States
Methalox (CH4 / LOX )
China
United States
Russia
Europe
Semi- cryogenic
Kerolox (RP-1 / LOX )
China
India
Russia
NK-15
NK-33, 44
RD-58
RD-0105, 0109
RD-0107, 0108, 0110
RD-0110R
RD-0124
RD-107, 108, 117, 118
RD-120
RD-170, 171
RD-180
RD-191, 151, 181
RD-193
S1.5400
Spain
Ukraine
United States
Storable
Hypergolic (Aerozine , UH 25 , MMH , or UDMH / N2 O4 , MON , or HNO3 )
China
Europe
India
Israel
North Korea
Russia
17D61
RD-0202 to 0206, 0208 to 0213
RD-0207, 0214
RD-0216, 0217, 0235
RD-0233, 0234
RD-0236
RD-0237
RD-0243 to 0245
RD-0255 to 0257
RD-215 to 219
RD-250 to 252, 261, 262
RD-253, 275
RD-263, 268, 273
RD-270
S5.92
S5.98M
Ukraine
United States
Other
Solid fuel
China
Europe
India
Iran
Israel
Japan
United States
* Different versions of the engine use different propellant combinations
Engines in italics are under development