A study of the boundary flow in a rocket combustion chamber. Part 3 - Data report Final report
Rocket motor boundary flow sampling apparatus
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Rocket motor boundary flow sampling apparatus
Mission and systems analyses for solar electric propulsion spacecraft flight to asteroid belt - Vol. 1
Asteroid belt mission using solar electric propulsion spacecraft - Vol. 2
Design and fabrication of conical wheels for lunar surface vehicle
Ben Franklin submersible use as space station analog
Feasibility and systems definition data for Orbiting Lunar Station
Design and development of reconfigurable guidance and control computer for space station applications - Vol. 2
Passive instrumentation and stimuli generation for Saturn IB equipment checkout - nondestructive testing
Chemical composition and mechanical properties of nickel maraging steel plate, forged, and weld wire materials for 260 inch diameter motor chamber and nozzle shell
Summary of Voyager spacecraft systems analysis and engineering tasks
Experiment designs for collecting human factors engineering data on advanced space systems maintenance
Neutral buoyancy simulation of zero gravity conditions encountered in space maintenance and repair
Astronaut EVA and IVA zero gravity performance
Comprehensive failure reporting of hardware and software problems for Earth Resources Technology Satellite
Two meter system for large telescope experiment program - summary
Apollo materials toxicity screening tests and effects of ethylene glycol, monomethylhydrazine, NF3, OF2, and ClF3
This is the thirteenth and final report in a series of TOPEX Radar Altimeter Engineering Assessment Reports. The initial TOPEX Radar Altimeter Engineering Assessment Report, in February 1994, presented performance results for the NASA Radar Altimeter on the TOPEX/POSEIDON spacecraft, from its launch in August 1992 to February 1994. Since the time of that initial report and prior to this report, there have been eleven interim supplemental Engineering Assessment Reports, issued in March 1995, May 1996, March 1997, June 1998, August 1999, September 2000, June 2001, March 2002, May 2003, April 2004 and September 2005. The sixth supplement in September 2000 was the first assessment report that addressed Side B performance, and presented the altimeter performance from Side B turn-on until the end of calendar year 1999. This report extends the performance assessment of Side B to the final collection of data on October 9, 2005, and includes the performance assessment of Jason-1, the TOPEX follow-on mission, launched on December 7, 2001. This report provides some comparisons of Side A and Side B performance.