0 citations
Orbiter Flash Evaporator: Flight Experience and Improvements
SAE technical papers on CD-ROM/SAE technical paper series1997Vol. 1
Citations Over Time
Abstract
<div class="htmlview paragraph">The Flash Evaporator Subsystem (FES) provides active cooling for the Shuttle Orbiter vehicle during the ascent and re-entry phases of the flight and provides supplemental cooling to the radiators while on-orbit. This paper describes the design and operation of the FES and summarizes the operational flight experience to date. As the fleet of orbiters grows older, contamination and corrosion are two issues on which attention has focused. A discussion of these conditions and the subsequent design changes and operational workarounds will be summarized.</div>
Related Papers
- → An empirical method for computing leeside centerline heating on the Space Shuttle Orbiter(1983)7 cited
- → Shuttle Orbiter Re-Entry Flowfields at High Angle of Attack(1973)4 cited
- → Errata-Experimental Dynamic Stability Characteristics of a Shuttle Orbiter at AL = 8(1976)3 cited
- Electrical power generation subsystem for Space Shuttle Orbiter(1974)
- Synergy Between Entry Probes and Orbiters(2005)