|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:check_in_time
|
8.5 minutes
|
|
gptkbp:control_system
|
digital
60% to 100%
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:designed_by
|
gptkb:Rocketdyne
|
|
gptkbp:development
|
1970s
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:durability
|
gptkb:true
|
|
gptkbp:engine
|
three
controlled
|
|
gptkbp:engine_configuration
|
vertical
|
|
gptkbp:engine_test
|
static fire
|
|
gptkbp:engine_type
|
gptkb:RS-25_A
gptkb:RS-25_D
gptkb:RS-25_E
gptkb:RS-25_B
gptkb:RS-25_C
gptkb:RS-25_F
gptkb:RS-25_G
gptkb:RS-25_H
gptkb:RS-25_I
gptkb:RS-25_J
gptkb:RS-25_K
gptkb:RS-25_L
gptkb:RS-25_M
gptkb:RS-25_N
gptkb:RS-25_P
gptkb:RS-25_Q
gptkb:RS-25_R
gptkb:RS-25_S
gptkb:RS-25_T
gptkb:RS-25_U
gptkb:RS-25_V
staged combustion
RS-25 O
RS-25 W
RS-25 X
RS-25 Y
RS-25 Z
|
|
gptkbp:exhaust_system
|
converging-diverging
|
|
gptkbp:first_flight
|
gptkb:1981
gptkb:2011
|
|
gptkbp:fuel_capacity
|
7.5 ft
14.5 ft
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
liquid hydrogen
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rocketdyne RS-25
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:launched
|
135
|
|
gptkbp:manufacturer
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:mission
|
gptkb:STS-1
|
|
gptkbp:number_of_engines
|
four
|
|
gptkbp:number_of_rooms
|
gptkb:single
70 psi
|
|
gptkbp:operational_period
|
closed cycle
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:propulsion
|
1900 lbf
|
|
gptkbp:related_vehicle
|
gptkb:Space_Launch_System
|
|
gptkbp:specific_impulse
|
452 seconds
|
|
gptkbp:successor
|
gptkb:RS-25_E
|
|
gptkbp:used_in
|
gptkb:Space_Shuttle
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:The_Space_Shuttle_Atlantis
|
|
gptkbp:bfsLayer
|
4
|