Template:Engine thrust to weight table

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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

Rocket thrusts are vacuum thrusts unless otherwise noted

References

  1. 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
  2. "«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0410. Nuclear Rocket Engine. Advanced launch vehicles". KBKhA - Chemical Automatics Design Bureau. Retrieved 2009-09-25.
  3. Aircraft: Lockheed SR-71A Blackbird
  4. "Factsheets : Pratt & Whitney J58 Turbojet". National Museum of the United States Air Force. Retrieved 2010-04-15.
  5. "ROLLS-ROYCE SNECMA OLYMPUS - Jane's Transport News". Retrieved 2009-09-25. With afterburner, reverser and nozzle ... 3,175 kg ... Afterburner ... 169.2 kN
  6. [1]
  7. 7.0 7.1 7.2 Military Jet Engine Acquisition, RAND, 2002.
  8. "«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0750". KBKhA - Chemical Automatics Design Bureau. Retrieved 2009-09-25.
  9. SSME
  10. "RD-180". Retrieved 2009-09-25.
  11. http://www.astronautix.com/engines/f1.htm
  12. Astronautix NK-33 entry

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