Properties (49)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft
|
| gptkbp:application |
space probes
satellite maneuvering launch vehicle upper stages orbital maneuvering |
| gptkbp:benefits |
toxic propellants
simple ignition process |
| gptkbp:characterizedBy |
ignition upon contact
|
| gptkbp:design |
system reliability
thrust vector control propellant compatibility |
| gptkbp:developer |
gptkb:European_Space_Agency
gptkb:Russian_space_program NASA |
| gptkbp:fuelType |
liquid
storable |
| gptkbp:futurePlans |
advanced propulsion systems
increased automation green propellants |
| gptkbp:historicalPeriod |
gptkb:Apollo_Lunar_Module
gptkb:Space_Shuttle_Orbital_Maneuvering_System gptkb:Mars_Rovers |
| https://www.w3.org/2000/01/rdf-schema#label |
Hypergolic thrusters
|
| gptkbp:is_used_in |
spacecraft propulsion
|
| gptkbp:keyFigures |
pumps
control systems valves nozzle heat exchangers ignition system fuel lines thrust chamber combustion chamber injectors propellant tanks |
| gptkbp:notableEvent |
Monomethylhydrazine_(MMH)
Nitrogen_tetroxide_(N2O4) |
| gptkbp:operationalStatus |
wide range
|
| gptkbp:performance |
thrust-to-weight ratio
specific impulse |
| gptkbp:researchFocus |
improving efficiency
enhancing safety reducing toxicity |
| gptkbp:safetyFeatures |
environmental impact
handling hazards |
| gptkbp:technology |
electric propulsion systems
bi-propellant engines monopropellant thrusters |
| gptkbp:uses |
hypergolic propellants
|