Command Module Service Propulsion System
GPTKB entity
Statements (47)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:consists_of |
reaction control system
main engine |
| gptkbp:control_system |
gptkb:sensors
|
| gptkbp:designed_by |
gptkb:North_American_Aviation
|
| gptkbp:developed_by |
1960s
|
| gptkbp:has_thrust |
16,000 pounds
|
| https://www.w3.org/2000/01/rdf-schema#label |
Command Module Service Propulsion System
|
| gptkbp:includes |
fuel tanks
oxidizer tanks |
| gptkbp:is_critical_for |
lunar missions
|
| gptkbp:is_designed_to |
provide propulsion
support crew safety control spacecraft orientation enable reentry |
| gptkbp:is_documented_in |
NASA archives
technical manuals engineering reports mission logs |
| gptkbp:is_evaluated_by |
performance metrics
safety assessments reliability tests efficiency tests |
| gptkbp:is_located_in |
gptkb:Public_service
|
| gptkbp:is_maintained_by |
NASA engineers
|
| gptkbp:is_part_of |
gptkb:Apollo_Lunar_Module
gptkb:Apollo_program |
| gptkbp:is_tested_for |
gptkb:NASA
thermal conditions vacuum conditions simulated space environment vibration conditions |
| gptkbp:is_used_for |
orbital maneuvers
lunar orbit insertion translunar injection deorbit burns |
| gptkbp:is_used_in |
gptkb:Apollo_11_mission
gptkb:Apollo_13_mission Apollo 17 mission |
| gptkbp:operates |
hypergolic propellants
|
| gptkbp:provides |
attitude control
thrust for spacecraft maneuvers |
| gptkbp:replaced_by |
modern spacecraft propulsion systems
|
| gptkbp:retired |
gptkb:1972
|
| gptkbp:used_by |
gptkb:Apollo_program
|
| gptkbp:bfsParent |
gptkb:James_Mc_Divitt
|
| gptkbp:bfsLayer |
5
|