Sycamore Captive Test Report for Missile 2D, S2-406-B3-02, S2-407-B3-02, S2-408-B3-02
Sycamore Captive Test Report for Missile 2D, S2-406-B3-02, S2-407-B3-02, S2-408-B3-02
Test B3, the first full duration static firing of a 'D' series missile, was successfully accomplished on 8 May 1959. The primary purposes of the test were to evaluate propulsion system performance, determine flight control system dynamic response and obtain data on airborne engine control pressurization during a full duration static firing.
Document information
Sycamore Captive Test Report for Missile 2D, S2-406-B3-02, S2-407-B3-02, S2-408-B3-02
1959
118 pages
Report
No indication
English
Rocket Engines & Motors , Missile Technology , Surface to surface missiles , Flight testing , Liquid propellant rocket engines , Simulation , Performance(Engineering) , Flight control systems , Response , Pressurization , Hydraulic equipment , Pneumatic devices , Captive tests , Electrical equipment , Telemetering data , Booster rockets , Sustainer engines , Vernier rocket engines , Atlas , Xsm-65d missiles
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