<?xml version="1.0"?>
<feed xmlns="http://www.w3.org/2005/Atom" xml:lang="en">
	<id>https://blackwiki.org/api.php?action=feedcontributions&amp;feedformat=atom&amp;user=64.236.5.4&amp;*</id>
	<title>blackwiki - User contributions [en]</title>
	<link rel="self" type="application/atom+xml" href="https://blackwiki.org/api.php?action=feedcontributions&amp;feedformat=atom&amp;user=64.236.5.4&amp;*"/>
	<link rel="alternate" type="text/html" href="https://blackwiki.org/index.php?title=Special:Contributions/64.236.5.4"/>
	<updated>2026-06-22T08:34:05Z</updated>
	<subtitle>User contributions</subtitle>
	<generator>MediaWiki 1.34.2</generator>
	<entry>
		<id>https://blackwiki.org/index.php?title=Template:Engine_thrust_to_weight_table&amp;diff=4844030</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=4844030"/>
		<updated>2013-08-28T01:04:48Z</updated>

		<summary type="html">&lt;p&gt;64.236.5.4: sort by thrust to weight&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{| class=&amp;quot;wikitable sortable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! [[Jet engine|Jet]] or [[Rocket engine|Rocket]] engine&lt;br /&gt;
! Mass&amp;lt;br/&amp;gt;(kg)&lt;br /&gt;
! Mass&amp;lt;br/&amp;gt;(lb)&lt;br /&gt;
! Thrust&amp;lt;br/&amp;gt;(kN)&lt;br /&gt;
! Thrust&amp;lt;br/&amp;gt;(lbf)&lt;br /&gt;
! [[Thrust-to-weight ratio]]&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;[http://www.marchfield.org/sr71a.htm Aircraft: Lockheed SR-71A Blackbird]&amp;lt;/ref&amp;gt;&amp;lt;ref&amp;gt;{{cite web| url=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}}&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 |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;astronautix1&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;
   |[[Space Shuttle Main Engine|SSME]] rocket engine ([[Space Shuttle]])&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&amp;lt;ref&amp;gt;{{cite news |title = SpaceX Unveils Plans To Be World’s Top Rocket Maker |url=http://www.aviationweek.com/publication/awst/loggedin/AvnowStoryDisplay.do?fromChannel=awst&amp;amp;pubKey=awst&amp;amp;channel=awst&amp;amp;issueDate=2011-08-08&amp;amp;story=xml/awst_xml/2011/08/08/AW_08_08_2011_p27-354586.xml&amp;amp;headline=SpaceX+Unveils+Plans+To+Be+World%26rsquo%3Bs+Top+Rocket+Maker |accessdate = 2012-10-11 |newspaper=Aviation Week and Space Technology |date=2011-08-11}}{{subscription required}}&amp;lt;/ref&amp;gt; &lt;br /&gt;
   |kg=440&lt;br /&gt;
   |kN=690&lt;br /&gt;
}}&lt;br /&gt;
|}&lt;br /&gt;
''Rocket thrusts are vacuum thrusts unless otherwise noted''&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>64.236.5.4</name></author>
		
	</entry>
	<entry>
		<id>https://blackwiki.org/index.php?title=Template:Engine_thrust_to_weight_table&amp;diff=4844029</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=4844029"/>
		<updated>2013-08-28T01:03:17Z</updated>

		<summary type="html">&lt;p&gt;64.236.5.4: add RD-170, most powerful engine ever&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{| class=&amp;quot;wikitable sortable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! [[Jet engine|Jet]] or [[Rocket engine|Rocket]] engine&lt;br /&gt;
! Mass&amp;lt;br/&amp;gt;(kg)&lt;br /&gt;
! Mass&amp;lt;br/&amp;gt;(lb)&lt;br /&gt;
! Thrust&amp;lt;br/&amp;gt;(kN)&lt;br /&gt;
! Thrust&amp;lt;br/&amp;gt;(lbf)&lt;br /&gt;
! [[Thrust-to-weight ratio]]&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;[http://www.marchfield.org/sr71a.htm Aircraft: Lockheed SR-71A Blackbird]&amp;lt;/ref&amp;gt;&amp;lt;ref&amp;gt;{{cite web| url=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}}&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 |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;astronautix1&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;
   |[[Space Shuttle Main Engine|SSME]] rocket engine ([[Space Shuttle]])&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;
   |[[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;
   |[[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;
   |[[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&amp;lt;ref&amp;gt;{{cite news |title = SpaceX Unveils Plans To Be World’s Top Rocket Maker |url=http://www.aviationweek.com/publication/awst/loggedin/AvnowStoryDisplay.do?fromChannel=awst&amp;amp;pubKey=awst&amp;amp;channel=awst&amp;amp;issueDate=2011-08-08&amp;amp;story=xml/awst_xml/2011/08/08/AW_08_08_2011_p27-354586.xml&amp;amp;headline=SpaceX+Unveils+Plans+To+Be+World%26rsquo%3Bs+Top+Rocket+Maker |accessdate = 2012-10-11 |newspaper=Aviation Week and Space Technology |date=2011-08-11}}{{subscription required}}&amp;lt;/ref&amp;gt; &lt;br /&gt;
   |kg=440&lt;br /&gt;
   |kN=690&lt;br /&gt;
}}&lt;br /&gt;
|}&lt;br /&gt;
''Rocket thrusts are vacuum thrusts unless otherwise noted''&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>64.236.5.4</name></author>
		
	</entry>
</feed>