A liquid injection thrust vector control (LITVC) system for the shuttle solid rocket booster (SRB) was analyzed. The LITVC was compared with the SRB baseline flexible seal. A table of LITVC advantages and disadvantages is presented. It is concluded that the LITVC performs well at low to moderate duty cycles, but not for high duty cycle requirements.
Feasibility study of LITVC for shuttle SRB
1981-09-01
Report
No indication
English
Shuttle seated extraction feasibility study
NTRS | 1989
|Feasibility Study of LITVC for Shuttle SRB
NTIS | 1981
|