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	<updated>2026-05-15T15:23:53Z</updated>
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	<entry>
		<id>https://blackwiki.org/index.php?title=Template:Engine_thrust_to_weight_table&amp;diff=4844041</id>
		<title>Template:Engine thrust to weight table</title>
		<link rel="alternate" type="text/html" href="https://blackwiki.org/index.php?title=Template:Engine_thrust_to_weight_table&amp;diff=4844041"/>
		<updated>2018-07-20T20:48:21Z</updated>

		<summary type="html">&lt;p&gt;200.3.250.240: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{| class=&amp;quot;wikitable sortable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! rowspan=2 | [[Jet engine|Jet]] or [[Rocket engine|rocket engine]]&lt;br /&gt;
! colspan=2 | Mass&lt;br /&gt;
! colspan=2 | Thrust (vacuum)&lt;br /&gt;
! rowspan=2 | [[Thrust-to-weight ratio]]&lt;br /&gt;
|-&lt;br /&gt;
! (kg)&lt;br /&gt;
! (lb)&lt;br /&gt;
! (kN)&lt;br /&gt;
! (lbf)&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[RD-0410]] nuclear rocket engine&amp;lt;ref name=&amp;quot;astronautix1&amp;quot;&amp;gt;{{cite web|url=http://www.astronautix.com/engines/rd0410.htm|title=RD-0410 |last=Wade|first=Mark|publisher=[[Encyclopedia Astronautica]]|accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;KBKhA-RD0410&amp;quot;&amp;gt;{{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&amp;amp;cat=11&amp;amp;prod=66 |accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=2000&lt;br /&gt;
   |kN=35.2&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[Pratt &amp;amp; Whitney J58|J58]] jet engine ([[Lockheed SR-71 Blackbird|SR-71 Blackbird]])&amp;lt;ref&amp;gt;{{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| deadurl=yes}}&amp;lt;/ref&amp;gt;&amp;lt;ref&amp;gt;{{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 &amp;amp; Whitney J58 Turbojet| publisher=National Museum of the United States Air Force| accessdate=2010-04-15| archivedate=2015-04-04| deadurl=yes}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=2722&lt;br /&gt;
   |kN=150&lt;br /&gt;
   |t/w=5.2&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   | [[Rolls-Royce/Snecma Olympus 593]]&amp;lt;br /&amp;gt;[[turbojet]] with reheat ([[Concorde]])&amp;lt;ref&amp;gt;{{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 |deadurl=yes |quote=With afterburner, reverser and nozzle ... 3,175 kg ... Afterburner ... 169.2 kN |accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=3175&lt;br /&gt;
   |kN=169.2&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row|[[Pratt &amp;amp; Whitney F119]]&amp;lt;ref&amp;gt;[http://www.rand.org/pubs/monograph_reports/2005/MR1596.pdf Military Jet Engine Acquisition], RAND, 2002.&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |lb=3900&lt;br /&gt;
   |lbf=20500&lt;br /&gt;
   |t/w=7.95&amp;lt;!-- apparent discrepancy in source, probably due to thrust in afterburner --&amp;gt;&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[RD-0750]] rocket engine, three-propellant mode&amp;lt;ref name=&amp;quot;KBKhA-RD0750&amp;quot;&amp;gt;{{cite web |title=«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0750. |publisher=KBKhA - [[Chemical Automatics Design Bureau]] |url=http://www.kbkha.ru/?p=8&amp;amp;cat=11&amp;amp;prod=57 |accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=4621&lt;br /&gt;
   |kN=1413&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[RD-0146]] rocket engine&amp;lt;ref name=&amp;quot;astronautix2&amp;quot;&amp;gt;{{cite web|url=http://www.astronautix.com/engines/rd0146.htm|title=RD-0146 |last=Wade|first=Mark|publisher=[[Encyclopedia Astronautica]]|accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=260&lt;br /&gt;
   |kN=98&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[Rocketdyne RS-25]] [[Space Shuttle]] [[Space Shuttle Main Engine|Main Engine]]&amp;lt;ref&amp;gt;[http://www.astronautix.com/engines/ssme.htm SSME]&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=3177&lt;br /&gt;
   |kN=2278&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[RD-180]] rocket engine&amp;lt;ref&amp;gt;{{cite web |title=RD-180 |publisher=|url=http://www.astronautix.com/engines/rd180.htm |accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=5393&lt;br /&gt;
   |kN=4152&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[RD-170]] rocket engine&lt;br /&gt;
   |kg=9750&lt;br /&gt;
   |kN=7887&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[F-1 (rocket engine)|F-1]] ([[Saturn V]] first stage)&amp;lt;ref&amp;gt;[http://www.astronautix.com/engines/f1.htm Encyclopedia Astronautica: F-1]&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=8391&lt;br /&gt;
   |kN=7740.5&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[NK-33]] rocket engine&amp;lt;ref name=&amp;quot;NK33&amp;quot;&amp;gt;[http://www.astronautix.com/engines/nk33.htm Astronautix NK-33 entry]&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=1222&lt;br /&gt;
   |kN=1638&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[Merlin 1D]] rocket engine, full-thrust version &amp;lt;ref name=&amp;quot;Merlin 1D&amp;quot;&amp;gt;{{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.}}&amp;lt;/ref&amp;gt; &lt;br /&gt;
   |kg=467&lt;br /&gt;
   |kN=825&lt;br /&gt;
}}&lt;br /&gt;
|}&amp;lt;noinclude&amp;gt;&lt;br /&gt;
{{template reference list}}&lt;br /&gt;
[[Category:Aviation templates]]&lt;br /&gt;
&amp;lt;/noinclude&amp;gt;&lt;/div&gt;</summary>
		<author><name>200.3.250.240</name></author>
		
	</entry>
	<entry>
		<id>https://blackwiki.org/index.php?title=Template:Engine_thrust_to_weight_table&amp;diff=4844040</id>
		<title>Template:Engine thrust to weight table</title>
		<link rel="alternate" type="text/html" href="https://blackwiki.org/index.php?title=Template:Engine_thrust_to_weight_table&amp;diff=4844040"/>
		<updated>2018-07-20T20:47:25Z</updated>

		<summary type="html">&lt;p&gt;200.3.250.240: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{| class=&amp;quot;wikitable sortable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! rowspan=2 | [[Jet engine|Jet]] or [[Rocket engine|rocket engine]]&lt;br /&gt;
! colspan=2 | Mass&lt;br /&gt;
! colspan=2 | Thrust (vacuum)&lt;br /&gt;
! rowspan=2 | [[Thrust-to-weight ratio]]&lt;br /&gt;
|-&lt;br /&gt;
! (kg)&lt;br /&gt;
! (lb)&lt;br /&gt;
! (kN)&lt;br /&gt;
! (lbf)&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[RD-0410]] nuclear rocket engine&amp;lt;ref name=&amp;quot;astronautix1&amp;quot;&amp;gt;{{cite web|url=http://www.astronautix.com/engines/rd0410.htm|title=RD-0410 |last=Wade|first=Mark|publisher=[[Encyclopedia Astronautica]]|accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=&amp;quot;KBKhA-RD0410&amp;quot;&amp;gt;{{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&amp;amp;cat=11&amp;amp;prod=66 |accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=2000&lt;br /&gt;
   |kN=35.2&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[Pratt &amp;amp; Whitney J58|J58]] jet engine ([[Lockheed SR-71 Blackbird|SR-71 Blackbird]])&amp;lt;ref&amp;gt;{{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| deadurl=yes}}&amp;lt;/ref&amp;gt;&amp;lt;ref&amp;gt;{{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 &amp;amp; Whitney J58 Turbojet| publisher=National Museum of the United States Air Force| accessdate=2010-04-15| archivedate=2015-04-04| deadurl=yes}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=2722&lt;br /&gt;
   |kN=150&lt;br /&gt;
   |t/w=5.2&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   | [[Rolls-Royce/Snecma Olympus 593]]&amp;lt;br /&amp;gt;[[turbojet]] with reheat ([[Concorde]])&amp;lt;ref&amp;gt;{{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 |deadurl=yes |quote=With afterburner, reverser and nozzle ... 3,175 kg ... Afterburner ... 169.2 kN |accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=3175&lt;br /&gt;
   |kN=169.2&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row|[[Pratt &amp;amp; Whitney F119]]&amp;lt;ref&amp;gt;[http://www.rand.org/pubs/monograph_reports/2005/MR1596.pdf Military Jet Engine Acquisition], RAND, 2002.&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |lb=3900&lt;br /&gt;
   |lbf=20500&lt;br /&gt;
   |t/w=7.95&amp;lt;!-- apparent discrepancy in source, probably due to thrust in afterburner --&amp;gt;&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[RD-0750]] rocket engine, three-propellant mode&amp;lt;ref name=&amp;quot;KBKhA-RD0750&amp;quot;&amp;gt;{{cite web |title=«Konstruktorskoe Buro Khimavtomatiky» - Scientific-Research Complex / RD0750. |publisher=KBKhA - [[Chemical Automatics Design Bureau]] |url=http://www.kbkha.ru/?p=8&amp;amp;cat=11&amp;amp;prod=57 |accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=4621&lt;br /&gt;
   |kN=1413&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[RD-0146]] rocket engine&amp;lt;ref name=&amp;quot;astronautix2&amp;quot;&amp;gt;{{cite web|url=http://www.astronautix.com/engines/rd0146.htm|title=RD-0146 |last=Wade|first=Mark|publisher=[[Encyclopedia Astronautica]]|accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=260&lt;br /&gt;
   |kN=98&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[Rocketdyne RS-25 Space Shuttle]] [[Space Shuttle Main Engine|Main Engine]]&amp;lt;ref&amp;gt;[http://www.astronautix.com/engines/ssme.htm SSME]&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=3177&lt;br /&gt;
   |kN=2278&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[RD-180]] rocket engine&amp;lt;ref&amp;gt;{{cite web |title=RD-180 |publisher=|url=http://www.astronautix.com/engines/rd180.htm |accessdate=2009-09-25}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=5393&lt;br /&gt;
   |kN=4152&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[RD-170]] rocket engine&lt;br /&gt;
   |kg=9750&lt;br /&gt;
   |kN=7887&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[F-1 (rocket engine)|F-1]] ([[Saturn V]] first stage)&amp;lt;ref&amp;gt;[http://www.astronautix.com/engines/f1.htm Encyclopedia Astronautica: F-1]&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=8391&lt;br /&gt;
   |kN=7740.5&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[NK-33]] rocket engine&amp;lt;ref name=&amp;quot;NK33&amp;quot;&amp;gt;[http://www.astronautix.com/engines/nk33.htm Astronautix NK-33 entry]&amp;lt;/ref&amp;gt;&lt;br /&gt;
   |kg=1222&lt;br /&gt;
   |kN=1638&lt;br /&gt;
}}&lt;br /&gt;
{{engine thrust to weight table/row&lt;br /&gt;
   |[[Merlin 1D]] rocket engine, full-thrust version &amp;lt;ref name=&amp;quot;Merlin 1D&amp;quot;&amp;gt;{{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.}}&amp;lt;/ref&amp;gt; &lt;br /&gt;
   |kg=467&lt;br /&gt;
   |kN=825&lt;br /&gt;
}}&lt;br /&gt;
|}&amp;lt;noinclude&amp;gt;&lt;br /&gt;
{{template reference list}}&lt;br /&gt;
[[Category:Aviation templates]]&lt;br /&gt;
&amp;lt;/noinclude&amp;gt;&lt;/div&gt;</summary>
		<author><name>200.3.250.240</name></author>
		
	</entry>
</feed>