Baseline: Centralized Control on Pumped LRB (1) Separate TVC and EC LRUs; (2) Analog TVC similar to SSME; (3) Orbiter Interface Assembly. Candidate 1: Centralized Control on Pressured LRB. (1) EC and TVC functions in on LRU. (2) Orbiter Interface Assembly. Candidate 2: Distributed Control on Pumped LRB. (1) Separate TVC and EC LRUs. (2) Digital TVC LRU interface. Candidate 3: Distributed Control on Pressured LRB. (1) EC and TVC in one LRU.
Liquid Rocket Booster (LRB) for the Space Transportation System (STS) Systems Study. Appendix I. Honeywell Avionics Trades Report
1989
154 pages
Report
No indication
English
Rocket Engines & Motors , Rocket Propellants , Booster rocket engines , Liquid rocket propellants , Planning , Schedules , Tasks , Chronology , Management , Space transportation system , Centralized control , Distributed control , Trade factors , Architecture characteristics , Terminal Voltage Control(TVC) , Liquid Rocket Booster(LRB) , Space Transportation System(STS)