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Ranking the Vulnerable Components of Aircraft by Considering Performance Degradations
Design and reliability considerations for the mariner mars 1964 spacecraft power system.
The requirements placed on electron tubes for space applications
Component performance and flight operations of the X-15 research airplane program.
Relative advantages of small and observatory type satellites
Some approximate methods for electric propulsion mission analysis.
Hitzefest. Design von Mixed-Signal-Hochtemperatur-ICs
Keine halben Sachen. Leistungsdichte und Performance von Automotive-Mosfets optimieren
Qualitätsmanagement in der Luftfahrtindustrie
Upscreening of microcircuits for military applications
Fatigue damage assessment of a car body-in-white using a frequency-domain approach
Quantifying Pilot Contribution to Flight Safety During an In-Flight Airspeed Failure
Lunar navigation study, sections 8 through 10 and appendices Final report, Jun. 1964 - May 1965
Test report for 3/8-inch relief valve Sage Engineering Company part number 1-2044
Exploring Propulsion System Requirements for More and All-Electric Helicopters
Exploring Propulsion System Requirements for More and All-Electric Helicopters