Difference between revisions of "Template:Engine thrust to weight table"
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imported>Mbeychok m (Deleted two broken/inactive reference links) |
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{{engine thrust to weight table/row | {{engine thrust to weight table/row | ||
| − | |[[Concorde]]'s [[Rolls-Royce/Snecma Olympus 593]]<br />[[turbojet]] with reheat<ref>{{cite web |title=ROLLS-ROYCE SNECMA OLYMPUS - Jane's Transport News |url=http://www.janes.com/transport/news/jae/jae000725_1_n.shtml |quote=With afterburner, reverser and nozzle ... 3,175 kg ... Afterburner ... 169.2 kN |accessdate=2009-09-25}} | + | |[[Concorde]]'s [[Rolls-Royce/Snecma Olympus 593]]<br />[[turbojet]] with reheat<ref>{{cite web |title=ROLLS-ROYCE SNECMA OLYMPUS - Jane's Transport News |url=http://www.janes.com/transport/news/jae/jae000725_1_n.shtml |quote=With afterburner, reverser and nozzle ... 3,175 kg ... Afterburner ... 169.2 kN |accessdate=2009-09-25}}</ref> |
|kg=3175 | |kg=3175 | ||
|kN=169.2 | |kN=169.2 | ||
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{{engine thrust to weight table/row | {{engine thrust to weight table/row | ||
| − | |[[Merlin 1D]] rocket engine | + | |[[Merlin 1D]] rocket engine |
|kg=440 | |kg=440 | ||
|kN=690 | |kN=690 | ||
Revision as of 16:51, 7 March 2013
| 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 |
| J-58 (SR-71 Blackbird jet engine)[3][4] | 2,722 | 6,001 | 150 | 34,000 | 5.2 |
| Concorde's Rolls-Royce/Snecma Olympus 593 turbojet with reheat[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[1] | 260 | 570 | 98 | 22,000 | 38.4 |
| Space Shuttle's SSME rocket engine[8] | 3,177 | 7,004 | 2,278 | 512,000 | 73.1 |
| RD-180 rocket engine[9] | 5,393 | 11,890 | 4,152 | 933,000 | 78.5 |
| F-1 (Saturn V first stage)[10] | 8,391 | 18,499 | 7,740.5 | 1,740,100 | 94.1 |
| NK-33 rocket engine[11] | 1,222 | 2,694 | 1,638 | 368,000 | 136.7 |
| Merlin 1D rocket engine | 440 | 970 | 690 | 160,000 | 159.9 |
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
- ↑ 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