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The RL60 is a rocket engine under development by Pratt and Whitney . The design is a high energy LH2/LOX expander cycle , capable of multiple restarts in space.
References
External links
Liquid fuel
Cryogenic
Hydrolox (LH2 / LOX )
China
Europe
India
Japan
Russia
USA
Methalox (CH4 / LOX )
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
USA
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
USA
Other
Solid fuel
China
Europe
India
Iran
Israel
Japan
USA
* Different versions of the engine use different propellant combinations
Engines in italics are under development