From Wikipedia, the free encyclopedia
American liquid rocket engine
The Rocketdyne S-3D is an American liquid rocket engine produced by Rocketdyne between 1956 and 1961 for use on the PGM-19 Jupiter and PGM-17 Thor missiles, and the Juno II rocket.[1][2] Its design was used later as the basis for the H-1 rocket engine of the Saturn I, and the Rolls-Royce RZ.2 of the Blue Streak.
It belongs to the LR79 engine family.[3]
- ^ Wade, Mark. "S-3D". Encyclopedia Astronautica. Archived from the original on November 7, 2016.
- ^ Wade, Mark. "Jupiter". Encyclopedia Astronautica. Archived from the original on October 10, 2011.
- ^ Wade, Mark. "LR79". Encyclopedia Astronautica. Retrieved 2024-07-29.
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Liquid fuel | Cryogenic | Hydrolox (LH2 / LOX) |
- China
- Europe
- India
- Japan
- Russia
- United States
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Methalox (CH4 / LOX) |
- China
- United States
- Russia
- Europe
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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
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Storable | Hypergolic (Aerozine, UH 25, MMH, or UDMH / N2O4, 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
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Other | |
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Solid fuel |
- China
- Europe
- India
- Iran
- Israel
- Japan
- United States
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- * Different versions of the engine use different propellant combinations
- Engines in italics are under development
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