American Redstone rocket engine
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:culturalHeritage |
derived from German V-2 engine
|
| gptkbp:cycle |
gas-generator cycle
|
| gptkbp:diameter |
1.8 m
|
| gptkbp:firstFlight |
1953
|
| gptkbp:fuelType |
ethyl alcohol
|
| gptkbp:gimbalRange |
5 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
American Redstone rocket engine
|
| gptkbp:length |
5.7 m
|
| gptkbp:manufacturer |
gptkb:North_American_Aviation
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
350 kN
|
| gptkbp:usedFor |
suborbital flights
ballistic missile launches manned spaceflight (Mercury-Redstone missions) |
| gptkbp:usedIn |
gptkb:Mercury-Redstone_Launch_Vehicle
gptkb:Redstone_missile |
| gptkbp:bfsParent |
gptkb:V-2_rocket_engine
|
| gptkbp:bfsLayer |
6
|