Determination of diaphragm opening-times and use of diaphragm particle traps in a hypersonic shock tube
Determination of diaphragm opening-times and use of diaphragm particle traps in hypersonic shock tube
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Determination of diaphragm opening-times and use of diaphragm particle traps in hypersonic shock tube
Tracking study to determine maximum control element lag and maximum and minimum control sensitivity tolerated in manually controlled compensatory tracking task
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This Technical Memorandum describes the Single Precision Orbit Determination Program which was developed for operation under the data processing system of the Space Flight Operations Facility. Included are sections containing flow diagrams, load maps, the common storage map, input and output descriptions, subroutine writeups, operating instructions, and check cases. The computational methods employed by the program are described in the subroutine documentation.
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