RL-10B-2 (Q31281957)

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model of rocket engine

RL10B-2
RL-10B-2-1
RL10B-2-1

Language	Label	Description	Also known as
English	RL-10B-2	model of rocket engine	RL10B-2 RL-10B-2-1 RL10B-2-1

Statements

0 references

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Delta IV rocket second stage.jpg
3,008 × 2,000; 812 KB

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301 kilogram

1 reference

https://www.nasa.gov/reference/space-launch-system-rl10-engine/

country of origin

United States of America

0 references

Pratt & Whitney

1 reference

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

1998

1 reference

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

4.15 metre

2 references

https://www.nasa.gov/reference/space-launch-system-rl10-engine/

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

2.146 metre

applies to part

rocket engine nozzle

2 references

https://www.nasa.gov/reference/space-launch-system-rl10-engine/

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

source of energy

1 reference

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

liquid hydrogen

1 reference

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

Delta Cryogenic Second Stage

0 references

Interim Cryogenic Propulsion Stage‎

object named as

ICPS-1

1 reference

https://www.nasa.gov/wp-content/uploads/2022/03/sls-reference-guide-2022-v2-508-0.pdf

9

110 kilonewton

1 reference

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

specific impulse by weight

465.5 second

1 reference

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

Sitelinks

Wikipedia(1 entry)

glwiki RL-10B-2

Wikibooks(0 entries)

Wikinews(0 entries)

Wikiquote(0 entries)

Wikisource(0 entries)

Wikiversity(0 entries)

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Wiktionary(0 entries)

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