Droplet combustion drop tower tests using models of the space flight apparatusAn engineering model built for droplet combustion drop tower tests is described. The model was built using a design with mechanical and electrical assemblies of the same level of complexity as they will have in flight. The model was tested for functional operation and integrated into a 5-sec drop tower. Test data obtained to date are presented together with model and test cell diagrams.
Document ID
19890041047
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Haggard, J. B. (NASA Lewis Research Center Cleveland, OH, United States)
Brace, M. H. (NASA Lewis Research Center Cleveland, OH, United States)
Kropp, J. L. (TRW, Inc. TRW Space and Technology Group, Redondo Beach, CA, United States)
Dryer, F. L. (Princeton University NJ, United States)