Reliability testing of the fault tolerant spacecraft computer (final rept.)
Reliability testing of a software-driven system
Reliability prediction of ETA (explosive transfer assembly) for the H-I launch vehicle
Reliability of periodic, coherent, binary systems
Reliability improvement warranty (RIW) and the army lightweight doppler navigation system (LDNS)
Reliability and safety analysis of a fault-tolerant controller
Reliability and quality requirements on microelectronics for space use
Reliability and flexibility of the IRAS on-board software
Reduce unconfirmed removals through mechanical design
Reconfigurable modular computer networks for spacecraft onboard processing
Quality measurement of mission critical systems
Progress in knowledge-based flight monitoring
Proc. of The Reliability Engng. Conf. For The Electr. Power Ind., New York, 21 February 1974