Difference between revisions of "Template:Engine thrust to weight table"

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m (Task 18a (cosmetic) (manual): eval 9 templates: del empty params (1×); hyphenate params (15×);)
 
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! (lbf)
 
! (lbf)
 
{{engine thrust to weight table/row
 
{{engine thrust to weight table/row
   |[[RD-0410]] nuclear rocket engine<ref name="astronautix1">{{cite web|url=http://www.astronautix.com/engines/rd0410.htm|title=RD-0410 |last=Wade|first=Mark|publisher=[[Encyclopedia Astronautica]]|accessdate=2009-09-25}}</ref><ref name="KBKhA-RD0410">{{cite web |title=«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0410. Nuclear Rocket Engine. Advanced launch vehicles |publisher=KBKhA - [[Chemical Automatics Design Bureau]] |url=http://www.kbkha.ru/?p=8&cat=11&prod=66 |accessdate=2009-09-25}}</ref>
+
   |[[RD-0410]] nuclear rocket engine<ref name="astronautix1">{{cite web|url=http://www.astronautix.com/engines/rd0410.htm|title=RD-0410 |last=Wade|first=Mark|publisher=[[Encyclopedia Astronautica]]|access-date=2009-09-25}}</ref><ref name="KBKhA-RD0410">{{cite web |title=«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0410. Nuclear Rocket Engine. Advanced launch vehicles |publisher=KBKhA - [[Chemical Automatics Design Bureau]] |url=http://www.kbkha.ru/?p=8&cat=11&prod=66 |access-date=2009-09-25}}</ref>
 
   |kg=2000
 
   |kg=2000
 
   |kN=35.2
 
   |kN=35.2
 
}}
 
}}
 
{{engine thrust to weight table/row
 
{{engine thrust to weight table/row
   |[[Pratt & Whitney J58|J58]] jet engine ([[Lockheed SR-71 Blackbird|SR-71 Blackbird]])<ref>{{cite web| url=http://www.marchfield.org/sr71a.htm| archiveurl=https://web.archive.org/web/20120729002902/http://www.marchfield.org/sr71a.htm| title=Aircraft: Lockheed SR-71A Blackbird| archivedate=2012-07-29| accessdate=2010-04-16| url-status=dead}}</ref><ref>{{cite web| url=http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=880 |archiveurl=https://web.archive.org/web/20150404113157/http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=880| title=Factsheets : Pratt & Whitney J58 Turbojet| publisher=National Museum of the United States Air Force| accessdate=2010-04-15| archivedate=2015-04-04| url-status=dead}}</ref>
+
   |[[Pratt & Whitney J58|J58]] jet engine ([[Lockheed SR-71 Blackbird|SR-71 Blackbird]])<ref>{{cite web| url=http://www.marchfield.org/sr71a.htm| archive-url=https://web.archive.org/web/20120729002902/http://www.marchfield.org/sr71a.htm| title=Aircraft: Lockheed SR-71A Blackbird| archive-date=2012-07-29| access-date=2010-04-16| url-status=dead}}</ref><ref>{{cite web| url=http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=880 |archive-url=https://web.archive.org/web/20150404113157/http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=880| title=Factsheets : Pratt & Whitney J58 Turbojet| publisher=National Museum of the United States Air Force| access-date=2010-04-15| archive-date=2015-04-04| url-status=dead}}</ref>
 
   |kg=2722
 
   |kg=2722
 
   |kN=150
 
   |kN=150
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}}
 
}}
 
{{engine thrust to weight table/row
 
{{engine thrust to weight table/row
   | [[Rolls-Royce/Snecma Olympus 593]]<br />[[turbojet]] with reheat ([[Concorde]])<ref>{{cite web |title=Rolls-Royce SNECMA Olympus - Jane's Transport News |url=http://www.janes.com/transport/news/jae/jae000725_1_n.shtml |archiveurl=https://web.archive.org/web/20100806140324/http://www.janes.com/transport/news/jae/jae000725_1_n.shtml| archivedate=2010-08-06 |url-status=dead |quote=With afterburner, reverser and nozzle ... 3,175 kg ... Afterburner ... 169.2 kN |accessdate=2009-09-25}}</ref>
+
   | [[Rolls-Royce/Snecma Olympus 593]]<br />[[turbojet]] with reheat ([[Concorde]])<ref>{{cite web |title=Rolls-Royce SNECMA Olympus - Jane's Transport News |url=http://www.janes.com/transport/news/jae/jae000725_1_n.shtml |archive-url=https://web.archive.org/web/20100806140324/http://www.janes.com/transport/news/jae/jae000725_1_n.shtml| archive-date=2010-08-06 |url-status=dead |quote=With afterburner, reverser and nozzle ... 3,175 kg ... Afterburner ... 169.2 kN |access-date=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
   |[[RD-0750]] rocket engine, three-propellant mode<ref name="KBKhA-RD0750">{{cite web |title=«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0750. |publisher=KBKhA - [[Chemical Automatics Design Bureau]] |url=http://www.kbkha.ru/?p=8&cat=11&prod=57 |accessdate=2009-09-25}}</ref>
+
   |[[RD-0750]] rocket engine, three-propellant mode<ref name="KBKhA-RD0750">{{cite web |title=«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0750. |publisher=KBKhA - [[Chemical Automatics Design Bureau]] |url=http://www.kbkha.ru/?p=8&cat=11&prod=57 |access-date=2009-09-25}}</ref>
 
   |kg=4621
 
   |kg=4621
 
   |kN=1413
 
   |kN=1413
 
}}
 
}}
 
{{engine thrust to weight table/row
 
{{engine thrust to weight table/row
   |[[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>
+
   |[[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]]|access-date=2009-09-25}}</ref>
 
   |kg=260
 
   |kg=260
 
   |kN=98
 
   |kN=98
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}}
 
}}
 
{{engine thrust to weight table/row
 
{{engine thrust to weight table/row
   |[[RD-180]] rocket engine<ref>{{cite web |title=RD-180 |publisher=|url=http://www.astronautix.com/engines/rd180.htm |accessdate=2009-09-25}}</ref>
+
   |[[RD-180]] rocket engine<ref>{{cite web |title=RD-180 |url=http://www.astronautix.com/engines/rd180.htm |access-date=2009-09-25}}</ref>
 
   |kg=5393
 
   |kg=5393
 
   |kN=4152
 
   |kN=4152
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}}
 
}}
 
{{engine thrust to weight table/row
 
{{engine thrust to weight table/row
   |[[Merlin 1D]] rocket engine, full-thrust version <ref name="Merlin 1D">{{cite web |last=Mueller |first=Thomas |title=Is SpaceX's Merlin 1D's thrust-to-weight ratio of 150+ believable? |url=https://www.quora.com/Is-SpaceXs-Merlin-1Ds-thrust-to-weight-ratio-of-150+-believable/answer/Thomas-Mueller-11 |accessdate=July 9, 2015 |date=June 8, 2015 |quote=The Merlin 1D weighs 1030 pounds, including the hydraulic steering (TVC) actuators.  It makes 162,500 pounds of thrust in vacuum.  that is nearly 158 thrust/weight.  The new full thrust variant weighs the same and makes about 185,500 lbs force in vacuum.}}</ref>  
+
   |[[Merlin 1D]] rocket engine, full-thrust version <ref name="Merlin 1D">{{cite web |last=Mueller |first=Thomas |title=Is SpaceX's Merlin 1D's thrust-to-weight ratio of 150+ believable? |url=https://www.quora.com/Is-SpaceXs-Merlin-1Ds-thrust-to-weight-ratio-of-150+-believable/answer/Thomas-Mueller-11 |access-date=July 9, 2015 |date=June 8, 2015 |quote=The Merlin 1D weighs 1030 pounds, including the hydraulic steering (TVC) actuators.  It makes 162,500 pounds of thrust in vacuum.  that is nearly 158 thrust/weight.  The new full thrust variant weighs the same and makes about 185,500 lbs force in vacuum.}}</ref>  
 
   |kg=467
 
   |kg=467
 
   |kN=825
 
   |kN=825

Latest revision as of 14:26, 21 December 2020

Jet or rocket engine Mass Thrust, vacuum Thrust-to-
weight ratio
(kg) (lb) (kN) (lbf)
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
Rocketdyne RS-25 rocket engine[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, full-thrust version [13] 467 1,030 825 185,000 180.1

References

  1. Wade, Mark. "RD-0410". Encyclopedia Astronautica. Retrieved 2009-09-25.
  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". Archived from the original on 2012-07-29. Retrieved 2010-04-16.
  4. "Factsheets : Pratt & Whitney J58 Turbojet". National Museum of the United States Air Force. Archived from the original on 2015-04-04. Retrieved 2010-04-15.
  5. "Rolls-Royce SNECMA Olympus - Jane's Transport News". Archived from the original on 2010-08-06. Retrieved 2009-09-25. With afterburner, reverser and nozzle ... 3,175 kg ... Afterburner ... 169.2 kN
  6. Military Jet Engine Acquisition, RAND, 2002.
  7. "«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0750". KBKhA - Chemical Automatics Design Bureau. Retrieved 2009-09-25.
  8. Wade, Mark. "RD-0146". Encyclopedia Astronautica. Retrieved 2009-09-25.
  9. SSME
  10. "RD-180". Retrieved 2009-09-25.
  11. Encyclopedia Astronautica: F-1
  12. Astronautix NK-33 entry
  13. Mueller, Thomas (June 8, 2015). "Is SpaceX's Merlin 1D's thrust-to-weight ratio of 150+ believable?". Retrieved July 9, 2015. The Merlin 1D weighs 1030 pounds, including the hydraulic steering (TVC) actuators. It makes 162,500 pounds of thrust in vacuum. that is nearly 158 thrust/weight. The new full thrust variant weighs the same and makes about 185,500 lbs force in vacuum.