RL-10 (Q967724): Difference between revisions

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Changed claim: length (P2043): 4.14 metre
Tag: Wikidata user interface
Huntster (talk | contribs)
 
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Property / imageProperty / image
Property / country
 
Property / country: United States of America / rank
Normal rank
 
Property / length
4.14 metre
Amount4.14 metre
Unitmetre
 
Property / length: 4.14 metre / rank
Normal rank
 
Property / diameter
2.13±0.01 metre
Amount2.13 metre
Upper bound2.14 metre
Lower bound2.12 metre
Unitmetre
 
Property / diameter: 2.13±0.01 metre / rank
Normal rank
 
Property / mass
277 kilogram
Amount277 kilogram
Unitkilogram
 
Property / mass: 277 kilogram / rank
Normal rank
 
Property / country of origin
 
Property / country of origin: United States of America / rank
 
Normal rank
Property / first flight
 
1961
Timestamp+1961-00-00T00:00:00Z
Zeitzone+00:00
CalendarGregorian
Precision1 year
Before0
After0
Property / first flight: 1961 / rank
 
Normal rank
Property / first flight: 1961 / reference
 
Property / has part(s)
 
Property / has part(s): RL-10A / rank
 
Normal rank
Property / has part(s)
 
Property / has part(s): RL-10B-2 / rank
 
Normal rank
Property / has part(s)
 
Property / has part(s): RL-10C / rank
 
Normal rank

Latest revision as of 10:07, 24 February 2024

liquid fuel cryogenic rocket engine, typically used on rocket upper stages
  • RL10
Sprache Label Description Also known as
Englisch
RL-10
liquid fuel cryogenic rocket engine, typically used on rocket upper stages
  • RL10

Statements

Identifiers