DocumentCode
1176330
Title
Gemini Titan II Booster Electrical System
Author
Sitter, Norman E.
Author_Institution
Martin Company Baltimore Division
Issue
4
fYear
1966
fDate
7/1/1966 12:00:00 AM
Firstpage
310
Lastpage
318
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;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1966.4501856
Filename
4501856
Link To Document