Reliability testing of the fault tolerant spacecraft computer (final rept.)
Proc. of The Reliability Engng. Conf. For The Electr. Power Ind., New York, 21 February 1974
Electronic delay ignition module for single bridgewire Apollo standard initiator
The national electrical code looks at aviation obstruction
Built-in-test in an ILS design-to-cost environment
Collision avoidance devices onboard U.S. navy ships (final rep. July 72 - July 74)
A digital computer simulation and study of a direct-energy-transfer power-conditioning system
Optimization of system reliability by branch-and-bound
Integrated flight control system design for CCV
Independent landing monitors / survey report
Analysis of pseudo-reliability of a combat tank system and its optimal design
TACAN and dual ILS station evaluation report. Randolph AFB, TX
Evaluating the GPSS simulation model for the Viking batch computer system
Doppler radars for low-cost, medium accuracy navigation
AGARD, Avionies Design for Reliability March 1976, Neuilly Sur Seine, France
Low-cost-high reliability keys to emergence of electronic computing for small engine control
Problems in determining an optimal electronic alerting and/or locating system
Indispensable components of a practical collision-free system Part II: The shape of things to come
Computer architectures for advanced air traffic control applications
VII, IFAC sympos. on automatic control in space, rottach-egern (FRG), 17-21 may, 1976
Introduction of the ground proximity warning system (GPWS) into airline service
A survey of primary radars for air traffic systems
Instrument landing system performance prediction
Embedded stress transducers for solid propellant rocket motor applications
Multiple access model for emergency position indicating radio beacons
'LEA' microwave approach and landing system
Designing a high-power, high-efficiency switching regulator for spacecraft applications
NASA's present and future sensor technology developments
A simulation technique in microprogram validation
Reliability improvement warranty (RIW) and the army lightweight doppler navigation system (LDNS)
Life cycle cost lessons learned from the standard electronic module radar program
Nuclear-powered infrared surveillance satellite study
Redundancy management of digital fly-by-wire systems
NASCAP, a three-dimensional charging analyzer program for complex spacecraft
What the courts say and have said about the use of radar (International maritime system)
Lifecycle testing for avionics development
Spacecraft charging characteristics and protection
Summary of the CTS transient event counter data after one year of operation