Reliability analysis of the Centaur IGS FIRST gimbal stabilization loop
Reliability analysis of Centaur inertial guidance system first gimbal stabilization loop
SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Reliability analysis of Centaur inertial guidance system first gimbal stabilization loop
Computer program to calculate probability of system success from arbitrary reliability block diagram using IBM 1620
Spacecraft power supply system and component reliability, efficiency, weight factors, and electromagnetic compatibility
Fuel cell acceptance, performance evaluation, and reliability testing
Reliability and failure mode prevention tests for Saturn integrated circuits
Comparison of some reliability growth estimation and prediction schemes
Gemini spacecraft reliability and quality control test program
Power system configurations and reliability for interplanetary missions to Mercury, Venus, Mars, and Jupiter
Reliability-confidence combinations for small sample tests of aerospace ordnance components
Preliminary power system configuration tradeoffs to select optimized systems with respect to reliability and weight - manual
Reliability analyses of global point-to-point communications system network for supporting manned and unmanned space missions
Reliability, planetary quarantine, support equipment, and interface alternatives of Voyager entry science package for Mars atmosphere probe
Voyager capsule surface laboratory system - reliability
Mariner IV Space Data Automation System /SDAS/ computer reliability design, pellet component concept, testing, interconnection and welding techniques
Relation between packaging design and cooling, vibration, RF interference and reliability of microelectronic systems used in space vehicles
Optimal allocation of n test points within redundant digital system for prelaunch and in-flight spacecraft reliability estimate
MORL system reliability analysis, discussing Monte Carlo simulation, major parameters, constraints, program contingencies, etc
Reliability criteria application to improvement of program and design decision quality during preliminary design