Missile 9A at Sycamore Test Stand S-1 is the last of the Series A captive missiles to be tested with the NAA B-2C booster engine. Block II was comprised of four tests, some of longer than full duration to accommodate autopilot testing programs. A total of 498 seconds of booster engine run time was accumulated to provide the environment for testing various missile systems and components. The primary areas of test interest centered about the flight control system, accessory power supply, telemetry system, missile component vibration and missile bending response during programmed gimbaling.
Data Survey Report for Sycamore Test Stand S-1 Block II Tests
1958
172 pages
Report
Keine Angabe
Englisch
Missile Technology , Rocket Engines & Motors , Surface to surface missiles , Captive tests , Booster rockets , Performance(Engineering) , Liquid propellant rocket engines , Servomechanisms , Frequency , Response , Hydraulic equipment , Telemeter systems , Reliability , Vibration , Bending , Automatic pilots , Power supplies , Flight control systems , Atlas , Graphs(Charts) , Xsm-65a missiles
Basic Captive Test Plan Sycamore Stand S-2
NTIS | 1956
|Sycamore Test Report TR-S1-301-A1-02
NTIS | 1958
|Sycamore Test Report TR-S1-301-A1-02
NTIS | 1958
|Engineering Index Backfile | 1955
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