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Einsatz zur Nutzanalyse fuer elektrische Triebwerke-Abschlussbericht
Electric Propulsion for Lunar Exploration and Lunar Base Development
Electric Thruster Power Conditioner Quarterly Technical Report, 1 Jul. - 30 Sep. 1968
Electron Bombardment Propulsion System Characteristics for Large Space Systems
EMI Performance of the AIRS Cooler and Electronics
EMP response of aircraft structures using transmission-line modelling
Endurance Evaluation of Long-Life Space Cryocoolers at AFRL—An Update
Engine knock detection with DSP microcontrollers
Engine Performance Monitoring with Cylinder Pressure Sensors
Erfahrungen bei der Untersuchung von Speicherbohrungen mittels Magnet-Impuls-Defektoskopie
Evaluation of Alternatives for Army Precision Landing System. Ground Guidance
Evaluation of a Platform Vertical Single-Component Thrust Stand
Evaluation of Metallized Propellants Based on Vehicle Performance
Evaluation of the WABCO AC Propulsion System. Volume 2. Related Reports and Exhibits
Evolution of satellite PFM encoding systems from 1960 to 1965
Evolution of standardized monopropellant rocket engine design concept
Exhaust Plume Characterization of a Mini-PPT Using a Time-of-Flight/ Gridded Energy Analyzer
Experimental Flow Characteristics Study of a High Frequency Pulse Tube Regenerator
Experimental Investigation of 4K VM Type Pulse Tube Cooler
Experimental Investigation of a G-M Type Coaxial Pulse Tube Cryocooler
Experimental Investigation of a Pulse Tube Refrigerator Driven by a Thermoacoustic Prime Mover
Experimental Investigation of a Unique Pulse Tube Expander Design
Experimental Investigation of Prepackaged Hybrid Propellant Systems
Experimental Investigation of Prepackaged Hybrid Propulsion Systems
Experimental Investigation of Unsteady Thrust Augmentation Using a Speaker-Driven Jet
Experimental investigations of momentum and heat transfer in pulse detonation engines
Experimental performance of a high specific impulse arc jet engine.
Experimental propulsion performance of a low power pulsed resistojet.
Experimental Results of Pulse Tube Cooler with Inertance Tube as Phase Shifter
Experimental Results on Inertance and Permanent Flow in Pulse Tube Coolers
Experimental Study of the Heat Transfer in Pulse Tubes
Experimental Study on Two-stage Pulse Tube Refrigeration with Mixtures of Helium and Hydrogen
Experimental Verification of a Thermodynamic Model for a Pulse Tube Cryocooler
Exploring in Aerospace Rocketry. 15 - Rocket Measurements and Instrumentation
External Pulsed Plasma Propulsion and Its Potential for the Near Future
Facility for Testing High-Power Electric Propulsion Systems in Space: A Design Study
Facility for the Evaluation of Space Communications and Related Systems
Fast and Efficient Collision Avoidance Algorithm for Autonomous Mobile Robot