11 research outputs found
Engine restart and thermodynamic analysis of Apollo spacecraft engine tests, volume 1
Thermodynamic performance test analyses for Apollo spacecraft ascent, descent, and service propulsion system engines to define hypergol engine restart limit
The influence of water vapor addition on hydrogen-oxygen detonations
http://deepblue.lib.umich.edu/bitstream/2027.42/5981/5/bac5840.0001.001.pdfhttp://deepblue.lib.umich.edu/bitstream/2027.42/5981/4/bac5840.0001.001.tx