The National Aeronautics and Space Administration needs to be sure the nozzles and heat shields of its new Space Launch System (SLS) rockets will be able to handle the heat generated during liftoff and ascent. Here, Kenyon discusses how engineers at Marshall Space Flight Center are turning to new tools and some Shuffle-era ones to measure the effects of the complicated heat flows that will envelope an SLS on every launch.
Modeling heat off rocket engines
Aerospace America ; 53 , 4
2015
Aufsatz (Zeitschrift)
Englisch
Heat transfer in rocket engines
TIBKAT | 1971
|Heat pipe cooled rocket engines
AIAA | 1986
|Heat pipe cooled rocket engines
NTRS | 1986
|NTIS | 1976
|