UNLIMITED FREE
ACCESS
TO THE WORLD'S BEST IDEAS

SUBMIT
Already a GlobalSpec user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your GlobalSpec Experience

Finish!
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

NASA-LLIS-0148

Lessons Learned - Reaction Control System (RCS) Thruster Valves

active, Most Current
Organization: NASA
Publication Date: 2 October 1992
Status: active
Page Count: 2
scope:

Description of Driving Event:

Leakage of small quantities of toxic propellants, monomethyl hydrazine (MMH) and nitrogen tetroxide (N2O4) from one or more reaction control system (RCS) thrusters could create an environment hazardous to personnel. The aft and forward RCS contain residual MMH and N2O4 under post-flight pressure. RCS thrusters have been known to leak when ambient temperature is low, orbiter valve pressure is low, and/or if there is no orbiter internal purge.

Document History

NASA-LLIS-0148
October 2, 1992
Lessons Learned - Reaction Control System (RCS) Thruster Valves
Description of Driving Event: Leakage of small quantities of toxic propellants, monomethyl hydrazine (MMH) and nitrogen tetroxide (N2O4) from one or more reaction control system (RCS) thrusters...
Advertisement