Statements (61)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:application |
spacecraft propulsion
|
| gptkbp:check_in_time |
approximately 1,000 seconds
|
| gptkbp:combustor_type |
staged combustion
|
| gptkbp:control_system |
manual control
|
| gptkbp:cooling_system |
regenerative cooling
effective cooling system |
| gptkbp:development |
gptkb:NASA
1960s |
| gptkbp:engine |
lightweight design
gas-generator cycle satellite propulsion autonomous operation advancements in rocket technology unique design features limited production run innovations in propulsion systems significant legacy in space exploration historically significant in aerospace history operational use in space missions rich history in aerospace engineering AJ10 series |
| gptkbp:engine_configuration |
single chamber
detailed specifications available Aerojet design |
| gptkbp:engine_contributions |
contributions to lunar missions
|
| gptkbp:engine_development_team |
dedicated development team
|
| gptkbp:engine_legacy_impact |
impact on future rocket designs
|
| gptkbp:engine_power |
high performance
high reliability high efficiency performance metrics documented retired after successful missions |
| gptkbp:engine_reliability_metrics |
reliability metrics documented
|
| gptkbp:engine_thrust_vector_control |
yes
|
| gptkbp:exhaust_system |
converging-diverging
|
| gptkbp:first_flight |
gptkb:1966
|
| gptkbp:fuel_capacity |
10 ft
3 ft |
| gptkbp:fuel_type |
hydrazine
hypergolic |
| https://www.w3.org/2000/01/rdf-schema#label |
Aerojet AJ10-138
|
| gptkbp:ignition_system |
hypergolic ignition
|
| gptkbp:is_tested_for |
extensive testing
NASA facilities |
| gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:mission |
Lunar landings
|
| gptkbp:number_of_rooms |
1,000 psi
|
| gptkbp:operational_status |
retired
|
| gptkbp:oxidation_states |
gptkb:nitrogen_tetroxide
hypergolic |
| gptkbp:propulsion |
gptkb:12.5
15,000 lbf |
| gptkbp:specific_impulse |
300 seconds
|
| gptkbp:successor |
AJ10-190
|
| gptkbp:type |
gptkb:Team_Rocket
|
| gptkbp:used_by |
gptkb:NASA
|
| gptkbp:used_in |
gptkb:Apollo_Lunar_Module
|
| gptkbp:weight |
1,200 lb
|
| gptkbp:bfsParent |
gptkb:Lunar_Module_3
|
| gptkbp:bfsLayer |
7
|