Difference between revisions of "Template:Engine thrust to weight table"
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imported>Monkbot m (Task 18a (cosmetic) (manual): eval 9 templates: del empty params (1×); hyphenate params (15×);) |
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! rowspan=2 | [[Jet engine|Jet]] or [[Rocket engine|rocket engine]] | ! rowspan=2 | [[Jet engine|Jet]] or [[Rocket engine|rocket engine]] | ||
! colspan=2 | Mass | ! colspan=2 | Mass | ||
| − | ! colspan=2 | Thrust | + | ! colspan=2 | Thrust, vacuum |
| − | ! rowspan=2 | [[Thrust-to-weight ratio]] | + | ! rowspan=2 | [[Thrust-to-weight ratio|Thrust-to-<br/>weight ratio]] |
|- | |- | ||
! (kg) | ! (kg) | ||
| Line 11: | Line 11: | ||
! (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]]| | + | |[[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| | + | |[[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 | ||
| Line 22: | Line 22: | ||
}} | }} | ||
{{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 | | + | | [[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 | ||
| Line 32: | Line 32: | ||
}} | }} | ||
{{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 | | + | |[[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]]| | + | |[[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 | ||
}} | }} | ||
{{engine thrust to weight table/row | {{engine thrust to weight table/row | ||
| − | |[[ | + | |[[Aerojet Rocketdyne|Rocketdyne]] [[RS-25]] rocket engine<ref>[http://www.astronautix.com/engines/ssme.htm SSME]</ref> |
|kg=3177 | |kg=3177 | ||
|kN=2278 | |kN=2278 | ||
}} | }} | ||
{{engine thrust to weight table/row | {{engine thrust to weight table/row | ||
| − | |[[RD-180]] rocket engine<ref>{{cite web |title=RD-180 | + | |[[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 | ||
| Line 67: | Line 67: | ||
}} | }} | ||
{{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 | | + | |[[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
- ↑ 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". Archived from the original on 2012-07-29. Retrieved 2010-04-16.
- ↑ "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.
- ↑ "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
- ↑ 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
- ↑ 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.