Pyrotechnics.
Pyrotechnic devices describing hot bridgewire, exploding bridgewire systems, mechanical and pressure actuated initiators and Gemini installations
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Pyrotechnic devices describing hot bridgewire, exploding bridgewire systems, mechanical and pressure actuated initiators and Gemini installations
Statistical analysis of pyrotechnic shock data from Ranger and Mariner test programs
Pyrotechnic shock isolation mount for protecting spacecraft equipment
Pyrotechnic shock analysis and testing methods for Ranger and Mariner spacecraft measurements
Heat sterilization of pyrotechnics and spacecraft onboard liquid and solid propulsion subsystems
System for measuring the output energy of pyrotechnic devices discharges the reaction products into a test chamber. It measures the radiant heat output from a pinhole aperture as well as internal pressure changes on a common time base.
Pyrotechnic heater provides a one-shot heat source capable of creating a predetermined temperature around sealed packages. It is composed of a blend of an active chemical element and another compound which reacts exothermically when ignited and produces fixed quantities of heat.
Pyrotechnic shock tests for Mariner Venus 67 flight acceptance
Pyrotechnic shaped charge aerospace vehicle stage and shroud separation systems development
Pyrotechnic-actuated calorimeter for flight research at lunar return velocity /Project Fire/
Premature actuation protection against RF interference for electroexplosive devices in spacecraft pyrotechnic systems
Pyrotechnic-activated heat-shield ejection system for NASA Project Fire
Pyrotechnic devices, functions, and systems for Apollo lunar landing
Pyrotechnic activated calorimeter for reentry package design of vehicles entering earth atmosphere at lunar return velocities
Apollo spacecraft pyrotechnics on lunar landing mission, considering standard initiator, modular cartridges, noninterchangeability of special purpose devices, postmanufacture indexing and data system
Apollo spacecraft pyrotechnic systems and devices functions during lunar exploration mission and in aborts
Characteristics of shock loads on spacecraft structures produced by pyrotechnics and explosive devices - Vol. 1
Pyrotechnic shock data associated with structure cutting charges consisting of mild detonating fuse and flexible linear shaped charge - Vol. 2