Difference between revisions of "Template:Engine thrust to weight table"
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imported>Mbeychok m (Expanded reference 11 (about the F-1) to eliminates the raw url.) |
imported>Jimp (Add the new subpage to calculate conversions & create rows.) |
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! [[Jet engine|Jet]] or [[Rocket engine|Rocket]] engine | ! [[Jet engine|Jet]] or [[Rocket engine|Rocket]] engine | ||
| − | ! Mass | + | ! Mass<br/>(kg) |
| − | ! | + | ! Mass<br/>(lb) |
| + | ! Thrust<br/>(kN) | ||
| + | ! Thrust<br/>(lbf) | ||
! [[Thrust-to-weight ratio]] | ! [[Thrust-to-weight ratio]] | ||
| − | + | {{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]]|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> |
| − | | 2000 | + | |kg=2000 |
| − | | 35.2 | + | |kN=35.2 |
| − | + | }} | |
| − | + | {{engine thrust to weight table/row | |
| − | | [[J-58]] ([[SR-71]] Blackbird jet engine)<ref>[http://www.marchfield.org/sr71a.htm Aircraft: Lockheed SR-71A Blackbird]</ref><ref>{{cite web| url=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}}</ref> | + | |[[J-58]] ([[SR-71]] Blackbird jet engine)<ref>[http://www.marchfield.org/sr71a.htm Aircraft: Lockheed SR-71A Blackbird]</ref><ref>{{cite web| url=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}}</ref> |
| − | | 2722 | + | |kg=2722 |
| − | | 150 | + | |kN=150 |
| − | | 5.2 | + | |t/w=5.2 |
| − | + | }} | |
| − | | [[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><ref> | + | {{engine thrust to weight table/row |
| − | | 3175 | + | |[[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><ref>http://www.faa.gov/about/office_org/headquarters_offices/AEP/supersonic_noise/media/1-Panel3-Brines_Smith-AADC.pdf</ref> |
| − | | 169.2 | + | |kg=3175 |
| − | + | |kN=169.2 | |
| − | + | }} | |
| − | | [[Pratt & Whitney F119]] | + | {{engine thrust to weight table/row|[[Pratt & Whitney F119]]<ref>[http://www.rand.org/pubs/monograph_reports/2005/MR1596.pdf Military Jet Engine Acquisition], RAND, 2002.</ref> |
| − | + | |lb=3900 | |
| − | | | + | |lbf=20500 |
| − | + | |t/w=7.95<!-- apparent discrepancy in source, probably due to thrust in afterburner --> | |
| − | + | }} | |
| − | | [[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> | + | {{engine thrust to weight table/row |
| − | | 4621 | + | |[[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> |
| − | | 1413 | + | |kg=4621 |
| − | + | |kN=1413 | |
| − | + | }} | |
| − | | [[RD-0146]] rocket engine<ref name="astronautix1">{{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> | + | {{engine thrust to weight table/row |
| − | | 260 | + | |[[RD-0146]] rocket engine<ref name="astronautix1">{{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> |
| − | | 98 | + | |kg=260 |
| − | + | |kN=98 | |
| − | + | }} | |
| − | | [[Space Shuttle]]'s [[Space Shuttle Main Engine|SSME]] rocket engine<ref>[http://www.astronautix.com/engines/ssme.htm SSME]</ref> | + | {{engine thrust to weight table/row |
| − | | 3177 | + | |[[Space Shuttle]]'s [[Space Shuttle Main Engine|SSME]] rocket engine<ref>[http://www.astronautix.com/engines/ssme.htm SSME]</ref> |
| − | | 2278 | + | |kg=3177 |
| − | + | |kN=2278 | |
| − | + | }} | |
| − | | [[RD-180]] rocket engine<ref>{{cite web |title=RD-180 |publisher=|url=http://www.astronautix.com/engines/rd180.htm |accessdate=2009-09-25}}</ref> | + | {{engine thrust to weight table/row |
| − | | 5393 | + | |[[RD-180]] rocket engine<ref>{{cite web |title=RD-180 |publisher=|url=http://www.astronautix.com/engines/rd180.htm |accessdate=2009-09-25}}</ref> |
| − | | 4152 | + | |kg=5393 |
| − | + | |kN=4152 | |
| − | + | }} | |
| − | |[[F-1 (rocket engine)|F-1]] ([[Saturn V]] first stage)<ref>[http://www.astronautix.com/engines/f1.htm Encyclopedia Astronautica: F-1]</ref> | + | {{engine thrust to weight table/row |
| − | |8391 | + | |[[F-1 (rocket engine)|F-1]] ([[Saturn V]] first stage)<ref>[http://www.astronautix.com/engines/f1.htm Encyclopedia Astronautica: F-1]</ref> |
| − | |7740.5 | + | |kg=8391 |
| − | + | |kN=7740.5 | |
| − | + | }} | |
| − | | [[NK-33]] rocket engine<ref name="NK33">[http://www.astronautix.com/engines/nk33.htm Astronautix NK-33 entry]</ref> | + | {{engine thrust to weight table/row |
| − | | 1222 | + | |[[NK-33]] rocket engine<ref name="NK33">[http://www.astronautix.com/engines/nk33.htm Astronautix NK-33 entry]</ref> |
| − | | 1638 | + | |kg=1222 |
| − | + | |kN=1638 | |
| − | + | }} | |
| − | | [[Merlin 1D]] rocket engine<ref name="Merlin 1D"> | + | {{engine thrust to weight table/row |
| − | | 440 | + | |[[Merlin 1D]] rocket engine<ref name="Merlin 1D">http://www.aviationweek.com/publication/awst/loggedin/AvnowStoryDisplay.do?fromChannel=awst&pubKey=awst&channel=awst&issueDate=2011-08-08&story=xml/awst_xml/2011/08/08/AW_08_08_2011_p27-354586.xml&headline=SpaceX+Unveils+Plans+To+Be+World%26rsquo%3Bs+Top+Rocket+Maker</ref> |
| − | | 690 | + | |kg=440 |
| − | + | |kN=690 | |
| + | }} | ||
|} | |} | ||
''Rocket thrusts are vacuum thrusts unless otherwise noted''<noinclude> | ''Rocket thrusts are vacuum thrusts unless otherwise noted''<noinclude> | ||
Revision as of 06:24, 20 September 2012
| 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][6] |
3,175 | 7,000 | 169.2 | 38,000 | 5.4 |
| Pratt & Whitney F119[7] | 1,800 | 3,900 | 91 | 20,500 | 7.95 |
| RD-0750 rocket engine, three-propellant mode[8] | 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[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 |
| 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 | 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
- ↑ http://www.faa.gov/about/office_org/headquarters_offices/AEP/supersonic_noise/media/1-Panel3-Brines_Smith-AADC.pdf
- ↑ 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
- ↑ http://www.aviationweek.com/publication/awst/loggedin/AvnowStoryDisplay.do?fromChannel=awst&pubKey=awst&channel=awst&issueDate=2011-08-08&story=xml/awst_xml/2011/08/08/AW_08_08_2011_p27-354586.xml&headline=SpaceX+Unveils+Plans+To+Be+World%26rsquo%3Bs+Top+Rocket+Maker