RL-10 (Q967724): Difference between revisions

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label / enlabel / en
RL10
RL-10
label / uklabel / uk
 
RL10
label / trlabel / tr
 
RL10
label / svlabel / sv
 
RL-10
label / gllabel / gl
 
RL-10
label / sllabel / sl
 
RL-10
aliases / en / 0aliases / en / 0
 
RL10
description / frdescription / fr
 
moteur-fusée à ergols liquides d'étages supérieurs
description / endescription / en
 
liquid fuel cryogenic rocket engine, typically used on rocket upper stages
description / fidescription / fi
 
rakettimoottori
description / dedescription / de
 
US-amerikanisches Raketentriebwerk
description / skdescription / sk
 
Kryogénny raketový motor na kvapalné palivo, zvyčajne používaný na horných stupňoch rakiet
description / svdescription / sv
 
raketmotor driven av flytande bränsle avsedd för slutsteg i raketer
description / sldescription / sl
 
kriogeni raketni motor na tekoče gorivo, ki se običajno uporablja za zgornje stopnje raket
Property / Commons categoryProperty / Commons category
RL10
RL10 (rocket engine)
Property / imageProperty / image
Property / country
 
Property / country: United States of America / rank
Normal rank
 
Property / manufacturer: Aerojet Rocketdyne / rankProperty / manufacturer: Aerojet Rocketdyne / rank
Normal rank
Preferred rank
Property / length
4.14±0.01 metre
Amount4.14 metre
Upper bound4.15 metre
Lower bound4.13 metre
Unitmetre
 
Property / length: 4.14±0.01 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±1 kilogram
Amount277 kilogram
Upper bound278 kilogram
Lower bound276 kilogram
Unitkilogram
 
Property / mass: 277±1 kilogram / rank
Normal rank
 
Property / instance of
 
Property / instance of: engine family / 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
links / frwiki / namelinks / frwiki / name
links / fiwiki / namelinks / fiwiki / name
links / itwiki / namelinks / itwiki / name
links / commonswiki / namelinks / commonswiki / name
 
links / ukwiki / namelinks / ukwiki / name
 
links / trwiki / namelinks / trwiki / name
 
links / svwiki / namelinks / svwiki / name
 
links / glwiki / namelinks / glwiki / name
 

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