(Q31281955)

English

RL-10A-4-2

model of rocket engine

RL10A-4-2

In more languages

Statements

0 references

0 references

167.8 kilogram

1 reference

https://www.l3harris.com/all-capabilities/rl10-engine

country of origin

United States of America

0 references

Pratt & Whitney

1 reference

http://astronautix.com/r/rl-10a-4-2.html

2002

1 reference

http://astronautix.com/r/rl-10a-4-2.html

2.29 metre

1 reference

https://www.l3harris.com/all-capabilities/rl10-engine

1.53 metre

applies to part

rocket engine nozzle

1 reference

http://astronautix.com/r/rl-10a-4-2.html

source of energy

1 reference

http://astronautix.com/r/rl-10a-4-2.html

liquid hydrogen

1 reference

http://astronautix.com/r/rl-10a-4-2.html

99.2 kilonewton

1 reference

https://www.l3harris.com/all-capabilities/rl10-engine

specific impulse by weight

451 second

1 reference

https://www.l3harris.com/all-capabilities/rl10-engine

Sitelinks

Wikipedia(1 entry)

glwiki RL-10A-4-2

Wikibooks(0 entries)

Wikinews(0 entries)

Wikiquote(0 entries)

Wikisource(0 entries)

Wikiversity(0 entries)

Wikivoyage(0 entries)

Wiktionary(0 entries)

Multilingual sites(0 entries)

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