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k Canister mating
Canister to adapter mating and ejection system
20 other sections not shown
15 July window 21 June 21 June window adapter Agena Agena-D albedo altitude analysis approximately August window axial axis battery packs bridge wire calculated canister assembly canister ejection system canister halves canister instrumentation canister opening system Canister Ring Separation components Condition Connector deployment determined dimple motors earth radiation ejection spring environmental equatorial flange explosive bolts external FLIGHT ACCEPTANCE ft/sec functions were monitored h August heat flux inch Instrumentation and Electrical instrumentation system launch vehicle leak rate load longitudinal lower half margin of safety minimum natural frequency node normal orbit PAGEOS pattern performed PETN plug Pogo Oscillations power cartridge Prototype patterns pyrotechnics qualification tests random vibration redundant Right ascension Ring Separation Test satellite shaped charge detonators shown in Figure shroud mount ring signal sinusoidal sliding valve slug ft.2 solar constant spacecraft strain gage structural surface Table tape telemetry Test Program Timer 83.5 second torr trajectory transducer transverse vacuum verify weight