Report ZM-7-602, Part 1, presents an evaluation of Composite Missile Systems Test FC-2C0-02-06, performed on Missile 6B in the Convair - Astronautics factory on 16 June 1958. Part 2 of Report ZM-7-602 presents results of acceptance testing of the Flight Control system on Missile 6B and includes completed data sheets from Flight Control Checkout Procedure 7-94001, Revision A. This addendum contains completed data sheets for all systems (except Flight Control) that were included in Composite Missile Systems Test FC-2C0-02-06. The Guidance and Impact Predictor systems (Procedures 7-94017 and 7-94076) and the Integrated Autopilot - Guidance systems (Procedure 7-94018) had not been accepted by AFQC at the time of publication. Completed data sheets from the composite missile systems test are included in Part 1 of ZM-7-602, together with Master Instrumentation Functional Checkout Guide (7-94065).
Factory Acceptance Testing Missile 6B. Completed Data Sheets
1958
81 pages
Report
Keine Angabe
Englisch
Missile Technology , Missile Trajectories & Reentry Dynamics , Quality Control & Reliability , Guided missile components , Acceptability , Surface to surface missiles , Checkout procedures , Telemeter systems , Electrical equipment , Guided missile safety , Rocket propulsion , Reliability , Flight control systems , Data , Atlas
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