Template:Engine thrust to weight table
Revision as of 03:32, 17 July 2012 by imported>Mbeychok (Expanded reference 11 (about the F-1) to eliminates the raw url.)
| Jet or Rocket engine | Mass, kg (lbs) | Jet or rocket thrust, kN (lbs) | Thrust-to-weight ratio |
|---|---|---|---|
| RD-0410 nuclear rocket engine[1][2] | 2000 | 35.2 | 1.8 |
| J-58 (SR-71 Blackbird jet engine)[3][4] | 2722 | 150 | 5.2 |
| Concorde's Rolls-Royce/Snecma Olympus 593 turbojet with reheat[5][6] |
3175 | 169.2 | 5.4 |
| Pratt & Whitney F119 | 1,800 (3,900)[7] | 91 (20,500)[7] | 7.95[7] |
| RD-0750 rocket engine, three-propellant mode[8] | 4621 | 1413 | 31.2 |
| RD-0146 rocket engine[1] | 260 | 98 | 38.5 |
| Space Shuttle's SSME rocket engine[9] | 3177 | 2278 | 73.2 |
| RD-180 rocket engine[10] | 5393 | 4152 | 78.6 |
| F-1 (Saturn V first stage)[11] | 8391 | 7740.5 | 94.1 |
| NK-33 rocket engine[12] | 1222 | 1638 | 136.8 |
| Merlin 1D rocket engine[13] | 440 | 690 | 160 |
Rocket thrusts are vacuum thrusts unless otherwise noted
References
- ↑ 1.0 1.1 Wade, Mark. "RD-0410". Encyclopedia Astronautica. Retrieved 2009-09-25. Cite error: Invalid
<ref>tag; name "astronautix1" defined multiple times with different content - ↑ "«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
- ↑ "Factsheets : Pratt & Whitney J58 Turbojet". National Museum of the United States Air Force. Retrieved 2010-04-15.
- ↑ "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]
- ↑ 7.0 7.1 7.2 Military Jet Engine Acquisition, RAND, 2002.
- ↑ "«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0750". KBKhA - Chemical Automatics Design Bureau. Retrieved 2009-09-25.
- ↑ SSME
- ↑ "RD-180". Retrieved 2009-09-25.
- ↑ Encyclopedia Astronautica: F-1
- ↑ Astronautix NK-33 entry
- ↑ [2]