|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:associated_missions
|
Gemini 3 to Gemini 12
|
|
gptkbp:challenges
|
high performance requirements
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:configuration
|
two-stage
|
|
gptkbp:contribution
|
gptkb:advanced_propulsion_systems
|
|
gptkbp:control_system
|
inertial guidance
|
|
gptkbp:debut
|
multiple launches
|
|
gptkbp:decommissioned
|
1990s
|
|
gptkbp:design_features
|
aerodynamic shape
|
|
gptkbp:development
|
1955-1962
|
|
gptkbp:diameter
|
10 ft
|
|
gptkbp:elevation
|
up to 200 km
|
|
gptkbp:engine
|
gptkb:LR87
|
|
gptkbp:engine_configuration
|
staged combustion
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:first_flight
|
gptkb:1962
gptkb:1986
numerous
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
kerosene and liquid oxygen
|
|
gptkbp:function
|
orbital insertion
|
|
gptkbp:guidance_system
|
inertial navigation
|
|
gptkbp:has_authority_over
|
pitch, yaw, roll
|
|
gptkbp:height
|
25 ft
|
|
gptkbp:historical_significance
|
pioneered crewed spaceflight
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Titan II second stage
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:influence
|
modern launch vehicles
|
|
gptkbp:integration
|
with Titan I
|
|
gptkbp:launch_date
|
frequent during operational years
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
|
|
gptkbp:launch_vehicle
|
gptkb:Titan_family
gptkb:Titan_II
|
|
gptkbp:legacy
|
influenced future rocket designs
|
|
gptkbp:manufacturer
|
gptkb:Martin_Marietta
|
|
gptkbp:mass
|
30,000 lb
|
|
gptkbp:mission
|
gptkb:1986
suborbital and orbital missions
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_cost
|
moderate
|
|
gptkbp:operational_period
|
1962-1986
|
|
gptkbp:operational_use
|
military and civilian missions
|
|
gptkbp:part_of
|
gptkb:Titan_II_rocket
|
|
gptkbp:payload_capacity
|
3,000 kg to low Earth orbit
shrouded payload
|
|
gptkbp:propulsion
|
gptkb:RP-1
3.67
liquid oxygen
110,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:safety_record
|
generally safe
|
|
gptkbp:significance
|
first stage to use RP-1 and LOX
|
|
gptkbp:stage_separation
|
mechanical separation
|
|
gptkbp:staging_event
|
after first stage burn
|
|
gptkbp:successor
|
gptkb:Titan_IV
|
|
gptkbp:used_in
|
gptkb:Gemini_program
|
|
gptkbp:bfsParent
|
gptkb:Titan_II
|
|
gptkbp:bfsLayer
|
5
|