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Captive Testing of Missile 14A at Mstsan-1, Edwards Air Force Base, Edwards, California
Discoverer Program Performance Analysis Report. Flight of FTV-1029. 13 August 1959 (30-Day Report)
Flight Performance of a Spin-Stabilized 20-Inch-Diameter Solid-Propellant Spherical Rocket Motor
SPACE VEHICLE ATTITUDE STABILIZATION USING PULSE-MODULATED JET CONTROL
Selection of Upper Stage Propulsion Systems for Space Vehicles
CONSIDERATION ON THE DESIGN OF PFM TELEMETRY ENCODERS
Physiologische Hitzeprobleme der Raumfahrt (Physiological Heating Problems of Space Flight)
NEL Constructed Prototype of the Sonar Target Converter
Payload Simulator Console. Part No. 1521003. Volume I
A DISCUSSION OF GUIDANCE POLICIES FOR MULTIPLE-IMPULSE CORRECTION OF THE TRAJECTORY OF A SPACECRAFT
Design and development of an integrated pulse modulated sixty pound thrust chamber Final report
DESIGN CRITERIA FOR ZERO-LEAKAGE CONNECTORS FOR LAUNCH VEHICLES, VOLUME 6 - ENVIRONMENTAL EFFECTS
The Resolution of Frequency Measurements in Pfm Telemetry
On the design of pfm telemetry encoders
The resolution of frequency measurements in pfm telemetry
Study of modulation techniques for multiple access satellite communications
Telemetry data processing plan for the OGO-A MISSION
Biomedical engineering units display systems for checkout and flight of gemini spacecraft.
Telemetry Data Processing Plan for the OGO-a Mission
Experimental performance of a high specific impulse arc jet engine.
Comparison of the Performance of PCM and Pfm Telemetry Systems
An on-off Control System for a Rotating Manned Spacecraft
An on-off control system for a rotating manned spacecraft
Changes in Pulse Rate Speed in Limbs Due to Age and Occupation
PCM telemetry data compression study, phase 1 Final report, 15 Sep. 1964 - 15 Aug. 1965
PCM Telemetry Data Compression Study, Phase 1 Final Report, 15 Sep. 1964 - 15 Aug. 1965
Experimental propulsion performance of a low power pulsed resistojet.
Study for a Flight Failure Warning and Analysis Pem System Final Report
Impulse and thrust test of a sublimating-solid micropropulsion system