The results of verification testing under NASA Contract NAS9-17249 are summarized in this Final Report. An Appendix is published separately. The report contains a brief discussion of design elements, test results, and a discussion of the latter. The contract was awarded for development and demonstration of design modifications to the NASA Standard Initiator-1 (NSI-1), resulting in the development of NSI-2. The intent of the project was to develop and prove the following design features: (1) Protection from premature initiation due to electrostatic potential by means other than a spark gap; (2) Development of an integral insulated charge cup for use with a zirconium/potassium perchlorate type mixture; (3) Improved cost and reliability figure...
Future spacecraft systems such as the manned space station will be subjected to low-dose long term r...
The analysis, design, fabrication, and testing of a propellant tank that satisfies the requirements ...
High strength aluminum alloy weldable in plate thicknesses for cryogenic temperature application
Test program for cap section mesh fabrication in prototype space erectable satellite developmen
This is the Appendix to the Final Report on the results of verification testing on NASA Contract NAS...
As part of the Civil Space Technology Initiative (CSTI) Advanced Technology program, a conceptual de...
Thermal analysis (BETA) computer program adaptations were prepared to analyze phase change histories...
Ring, brush, and insulator materials effect on electrical noise and mechanical wear characteristics ...
Thermal energy storage (TES) enables a solar dynamic system to deliver constant electric power throu...
Explosive charges of various sizes were investigated for use in lunar seismic studies. Program logis...
Space shuttle high pressure, hydrogen oxygen auxiliary propulsion subsystem preliminary desig
Several approaches to develop a diagnostics system for monitoring the operational health of the Spac...
Progress in robust design of generalized parity relations, design of failure sensitive observers usi...
Electronic instrumentation and procedures for environmental and reliability testing of UK-2/S-52 int...
The engineering model resistojet intended for altitude maintenance onboard the space station was tes...
Future spacecraft systems such as the manned space station will be subjected to low-dose long term r...
The analysis, design, fabrication, and testing of a propellant tank that satisfies the requirements ...
High strength aluminum alloy weldable in plate thicknesses for cryogenic temperature application
Test program for cap section mesh fabrication in prototype space erectable satellite developmen
This is the Appendix to the Final Report on the results of verification testing on NASA Contract NAS...
As part of the Civil Space Technology Initiative (CSTI) Advanced Technology program, a conceptual de...
Thermal analysis (BETA) computer program adaptations were prepared to analyze phase change histories...
Ring, brush, and insulator materials effect on electrical noise and mechanical wear characteristics ...
Thermal energy storage (TES) enables a solar dynamic system to deliver constant electric power throu...
Explosive charges of various sizes were investigated for use in lunar seismic studies. Program logis...
Space shuttle high pressure, hydrogen oxygen auxiliary propulsion subsystem preliminary desig
Several approaches to develop a diagnostics system for monitoring the operational health of the Spac...
Progress in robust design of generalized parity relations, design of failure sensitive observers usi...
Electronic instrumentation and procedures for environmental and reliability testing of UK-2/S-52 int...
The engineering model resistojet intended for altitude maintenance onboard the space station was tes...
Future spacecraft systems such as the manned space station will be subjected to low-dose long term r...
The analysis, design, fabrication, and testing of a propellant tank that satisfies the requirements ...
High strength aluminum alloy weldable in plate thicknesses for cryogenic temperature application