Title :
Gemini Titan II Booster Electrical System
Author :
Sitter, Norman E.
Author_Institution :
Martin Company Baltimore Division
fDate :
7/1/1966 12:00:00 AM
Abstract :
A description of the Gemini Titan II Launch Vehicle´s redundant electrical system and differences between the electrical systems of the Titan II and Gemini Titan II Launch Vehicles are presented. Also described are the interfaces with the guidance/flight control, malfunction detection, range safety, hydraulic and instrumentation systems, and the interface of the launch vehicle and Gemini spacecraft. Principal electrical component characteristics are presented, and data obtained during flight is compared with that obtained during ground checkout.
Keywords :
Aerospace control; Aerospace safety; Electrical safety; Instruments; Navigation; Power systems; Relays; Space vehicles; Switches; Vehicle safety;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.1966.4501856
