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, kg (lbs)
+
! Mass<br/>(kg)
! Jet or rocket thrust, kN (lbs)
+
! 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
| {{#expr: 35.2 / (2.000 * 9.8) round 1}}
+
}}
|-
+
{{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>[http://www.faa.gov/about/office_org/headquarters_offices/AEP/supersonic_noise/media/1-Panel3-Brines_Smith-AADC.pdf]</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
| {{#expr: 169.2 / (3.175 * 9.8) round 1}}
+
  |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>
| {{convert|3900|lb|kg|disp=flip|abbr=values}}<ref name=Rand>[http://www.rand.org/pubs/monograph_reports/2005/MR1596.pdf Military Jet Engine Acquisition], RAND, 2002.</ref>
+
  |lb=3900
| {{convert|20500|lbf|kN|disp=flip|abbr=values}}<ref name=Rand/>
+
  |lbf=20500
| 7.95<ref name=Rand/> <!-- apparent discrepancy in source, probably due to thrust in afterburner -->
+
  |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
| {{#expr: 1413 / (4.621 * 9.8) round 1}}
+
  |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
| {{#expr: 98 / (.260 * 9.8) round 1}}
+
  |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
| {{#expr: 2278 / (3.177 * 9.8) round 1}}
+
  |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
| {{#expr: 4152 / (5.393 * 9.8) round 1}}
+
  |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
|{{#expr: 7740.5 / (8.391 * 9.8) round 1}}
+
  |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
| {{#expr: 1638 / (1.222 * 9.8) round 1}}
+
  |kN=1638
|-
+
}}
| [[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>
+
{{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
| {{#expr: 690 / (0.440 * 9.8) round 1}}
+
  |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. 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. http://www.faa.gov/about/office_org/headquarters_offices/AEP/supersonic_noise/media/1-Panel3-Brines_Smith-AADC.pdf
  7. 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. Encyclopedia Astronautica: F-1
  12. Astronautix NK-33 entry
  13. 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

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