Accession Number : AD0829589
Title : DATA SURVEY REPORT FOR SYCAMORE TEST STAND S-1 BLOCK II TESTS,
Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Personal Author(s) : Eldridge, H. P.
Report Date : 03 APR 1958
Pagination or Media Count : 172
Abstract : 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.
Descriptors : (*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.
Subject Categories : Surface-launched Guided Missiles
Liquid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE