Home
Random
Nearby
Log in
Settings
Donate
About Wikidata
Disclaimers
Search
(Q31281956)
Watch
English
RL-10A-5
model of rocket engine
RL10A-5
In more languages
default for all languages
No label defined
No description defined
edit
Statements
instance of
engine model
0 references
subclass of
RL-10A
0 references
mass
143
kilogram
1 reference
reference URL
http://astronautix.com/r/rl-10a-5.html
country of origin
United States of America
0 references
manufacturer
Pratt & Whitney
1 reference
reference URL
http://astronautix.com/r/rl-10a-5.html
first flight
1993
1 reference
reference URL
http://astronautix.com/r/rl-10a-5.html
height
1.07
metre
1 reference
reference URL
http://astronautix.com/r/rl-10a-5.html
diameter
1.02
metre
1 reference
reference URL
http://astronautix.com/r/rl-10a-5.html
source of energy
liquid oxygen
1 reference
reference URL
http://astronautix.com/r/rl-10a-5.html
liquid hydrogen
1 reference
reference URL
http://astronautix.com/r/rl-10a-5.html
used by
McDonnell Douglas DC-X
0 references
maximum thrust
64.70
kilonewton
1 reference
reference URL
http://astronautix.com/r/rl-10a-5.html
specific impulse by weight
316
second
applies to part
sea level
1 reference
reference URL
http://astronautix.com/r/rl-10a-5.html
Sitelinks
Wikipedia
(1 entry)
edit
glwiki
RL-10A-5
Wikibooks
(0 entries)
edit
Wikinews
(0 entries)
edit
Wikiquote
(0 entries)
edit
Wikisource
(0 entries)
edit
Wikiversity
(0 entries)
edit
Wikivoyage
(0 entries)
edit
Wiktionary
(0 entries)
edit
Multilingual sites
(0 entries)
edit