Difference between revisions of "Template:Engine thrust to weight table"
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| − | |[[RD-0146]] rocket engine<ref name=" | + | |[[RD-0146]] rocket engine<ref name="astronautix2">{{cite web|url=http://www.astronautix.com/engines/rd0146.htm|title=RD-0146 |last=Wade|first=Mark|publisher=[[Encyclopedia Astronautica]]|accessdate=2009-09-25}}</ref> |
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Revision as of 22:16, 17 October 2015
| Jet or Rocket engine | Mass (kg) |
Mass (lb) |
Thrust (kN) |
Thrust (lbf) |
Thrust-to-weight ratio |
|---|---|---|---|---|---|
| RD-0410 nuclear rocket engine[1][2] | 2,000 | 4,400 | 35.2 | 7,900 | 1.8 |
| J58 jet engine (SR-71 Blackbird)[3][4] | 2,722 | 6,001 | 150 | 34,000 | 5.2 |
| Rolls-Royce/Snecma Olympus 593 turbojet with reheat (Concorde)[5] |
3,175 | 7,000 | 169.2 | 38,000 | 5.4 |
| Pratt & Whitney F119[6] | 1,800 | 3,900 | 91 | 20,500 | 7.95 |
| RD-0750 rocket engine, three-propellant mode[7] | 4,621 | 10,188 | 1,413 | 318,000 | 31.2 |
| RD-0146 rocket engine[8] | 260 | 570 | 98 | 22,000 | 38.4 |
| SSME rocket engine (Space Shuttle)[9] | 3,177 | 7,004 | 2,278 | 512,000 | 73.1 |
| RD-180 rocket engine[10] | 5,393 | 11,890 | 4,152 | 933,000 | 78.5 |
| RD-170 rocket engine | 9,750 | 21,500 | 7,887 | 1,773,000 | 82.5 |
| F-1 (Saturn V first stage)[11] | 8,391 | 18,499 | 7,740.5 | 1,740,100 | 94.1 |
| NK-33 rocket engine[12] | 1,222 | 2,694 | 1,638 | 368,000 | 136.7 |
| Merlin 1D rocket engine[13] | 440 | 970 | 716 | 161,000 | 165.9 |
Rocket thrusts are vacuum thrusts unless otherwise noted
References
- ↑ Wade, Mark. "RD-0410". Encyclopedia Astronautica. Retrieved 2009-09-25.
- ↑ "«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
- ↑ Military Jet Engine Acquisition, RAND, 2002.
- ↑ "«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0750". KBKhA - Chemical Automatics Design Bureau. Retrieved 2009-09-25.
- ↑ Wade, Mark. "RD-0146". Encyclopedia Astronautica. Retrieved 2009-09-25.
- ↑ SSME
- ↑ "RD-180". Retrieved 2009-09-25.
- ↑ Encyclopedia Astronautica: F-1
- ↑ Astronautix NK-33 entry
- ↑ Taylor, John. "Press Kit – June 2015 SpaceX CRS-7 Mission Cargo Resupply Services". NASA. pp. 17–18. Archived from the original (PDF) on 2015-06-27. Retrieved 28 June 2015. Unknown parameter
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