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LIQUID-PROPELLANT ROCKET ENGINE [1 record]
Record 1 - internal organization data 2012-07-12
Record 1, English
Record 1, Subject field(s)
- Missiles and Rockets
- Spacecraft
- Launchers (Astronautics)
Record 1, Main entry term, English
- liquid-propellant rocket engine
1, record 1, English, liquid%2Dpropellant%20rocket%20engine
correct
Record 1, Abbreviations, English
Record 1, Synonyms, English
- liquid propellant engine 2, record 1, English, liquid%20propellant%20engine
correct
- liquid-propellant engine 3, record 1, English, liquid%2Dpropellant%20engine
correct
- liquid propellant motor 4, record 1, English, liquid%20propellant%20motor
correct
- liquid-propellant motor 5, record 1, English, liquid%2Dpropellant%20motor
correct
Record 1, Textual support, English
Record number: 1, Textual support number: 1 OBS
rocket engine: A propulsive device in which liquid propellants are burnt in a combustion chamber to provide a reaction force to propel the vehicle. 6, record 1, English, - liquid%2Dpropellant%20rocket%20engine
Record 1, Key term(s)
- liquid propellant rocket engine
Record 1, French
Record 1, Domaine(s)
- Missiles et roquettes
- Engins spatiaux
- Lanceurs (Astronautique)
Record 1, Main entry term, French
- propulseur à liquide
1, record 1, French, propulseur%20%C3%A0%20liquide
correct, masculine noun
Record 1, Abbreviations, French
Record 1, Synonyms, French
- moteur-fusée à propergol liquide 1, record 1, French, moteur%2Dfus%C3%A9e%20%C3%A0%20propergol%20liquide
correct, masculine noun
- système de propulsion à propergols liquides 2, record 1, French, syst%C3%A8me%20de%20propulsion%20%C3%A0%20propergols%20liquides
correct, masculine noun
- système de propulsion à ergols liquides 3, record 1, French, syst%C3%A8me%20de%20propulsion%20%C3%A0%20ergols%20liquides
correct, masculine noun
Record 1, Textual support, French
Record number: 1, Textual support number: 1 DEF
Propulseur fonctionnant au moyen d'ergols liquides ou en bouillie. 1, record 1, French, - propulseur%20%C3%A0%20liquide
Record number: 1, Textual support number: 1 CONT
Les caractéristiques principales du missile (XMGM-52C Lance) sont un système de guidage inertiel et un système de propulsion à propergols liquides, qui ont, l'un et l'autre, été spécifiquement développés pour le doter d'une précision et d'une fiabilité comparables à celles de l'artillerie de campagne classique. 2, record 1, French, - propulseur%20%C3%A0%20liquide
Record 1, Spanish
Record 1, Textual support, Spanish
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