Template:Engine thrust to weight table: Difference between revisions
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|[[F-1 (rocket engine)|F-1]] ([[Saturn V]] first stage) |
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| [[NK-33]] rocket engine sea-level<ref name="NK33"/> |
| [[NK-33]] rocket engine sea-level<ref name="NK33"/> |
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Revision as of 11:18, 19 October 2009
| Jet or Rocket engine | Mass, kg | Jet or rocket thrust, kN | Thrust-to-weight ratio |
|---|---|---|---|
| RD-0410 nuclear rocket engine[1][2] | 2000 | 35.2 | 1.8 |
| J-58 (SR-71 Blackbird jet engine)[3] | 5.2 | ||
| Concorde's Rolls-Royce/Snecma Olympus 593 turbojet with reheat[4][5] |
3175 | 169.2 | 5.4 |
| RD-0750 rocket engine, three-propellant mode[6] | 4621 | 1413 | 31.2 |
| RD-0146 rocket engine[1] | 260 | 98 | 38.5 |
| Space shuttle's SSME rocket engine[7] | 73.12 | ||
| RD-180 rocket engine[8] | 5393 | 4152 | 78.6 |
| F-1 (Saturn V first stage) | 8391 | 6770 | 82.3 |
| NK-33 rocket engine sea-level[9] | 1222 | 1510 | 126.1 |
| NK-33 rocket engine vaccum[9] | 1222 | 1638 | 136.8 |
Rocket thrusts are vaccuum thrusts unless otherwise noted
- ^ a b Wade, Mark. "RD-0410". Encyclopedia Astronautica. Retrieved 2009-09-25. Cite error: The named reference "astronautix1" was defined multiple times with different content (see the help page).
- ^ "«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0410. Nuclear Rocket Engine. Advanced launch vehicles". KBKhA - Chemical Automatics Design Bureau. Retrieved 2009-09-25.
- ^ Aircraft: Lockheed SR-71A Blackbird
- ^ "ROLLS-ROYCE SNECMA OLYMPUS - Jane's Transport News". Retrieved 2009-09-25.
With afterburner, reverser and nozzle ... 3,175 kg ... Afterburner ... 169.2 kN
- ^ [1]
- ^ "«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0750". KBKhA - Chemical Automatics Design Bureau. Retrieved 2009-09-25.
- ^ SSME
- ^ "RD-180". Retrieved 2009-09-25.
- ^ a b Astronautix NK-33 entry