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Design Issues for Propulsion Systems Using Metallized Propellants
Design of permanent magnet synchronous machines for self-sensing control in electric vehicles
Design of the EO-1 Pulsed Plasma Thruster Attitude Control Experiment
Detection of Damaged Distribution Surge Arresters Using an Impulse Generator
Development of 40–80K Linear-Compressor Driven Pulse Tube Cryocoolers
Development of a 1 to 5 W at 80 K Stirling Pulse Tube Cryocooler
Development of a 2 W at 60 K Pulse Tube Cryocooler for Spaceborne Operation
Development of a 4K Two-stage Pulse Tube Cryocooler
Development of a 5 to 20 W at 80 K GM Pulse Tube Cryocooler
Development of a 5W at 65 K Air-Cooled Pulse Tube Cryocooler
Development of a 5 W at 80 K Stirling-Type Pulse Tube Cryocooler
Development of a 10 K Pulse Tube Cryocooler for Space Applications
Development of a 13 kW Hall Thruster Propulsion System Performance Model for AEPS
Development of a GM-Type Pulse Tube Refrigerator Cooling System for Superconducting Maglev Vehicles
Development of a High Capacity Two-Stage Pulse Tube Cryocooler
Development of a Lightweight Pulse Tube Cryocooler for Space Applications
Development of a Long-Life Stirling Pulse Tube Cryocooler for a Superconducting Filter Subsystem
Development of a Prototype Rocket Engine for a Nanosat Launch Vehicle First Stage (Preprint)
Development of Arcjet and Ion Propulsion for Spacecraft Stationkeeping
Development of a Single Stage Pulse Tube Refrigerator with Linear Compressor
Development of a Two-Stage Pulse Tube Cryocooler for 35 K Cooling
Development of Checkout Specifications for New Telemeter Systems, Phase B
Development of K. E. Tsiolkovskiy's Ideas about the Use of Air Breathing Jet Engines on Rockets
Development of Pulse Tube Cryocoolers for HTS Satellite Communications
Development of Single and Two-Stage Pulse Tube Cryocoolers with Commercial Linear Compressors
Development of Stirling-Type Coaxial Pulse Tube Cryocoolers
Development of the LSF95xx 2nd Generation Flexure Bearing Coolers
Development of the TC-101 Ionosphere Timing and Control Unit
Developments on Single and Double Stage GM Type Pulse Tube Cryorefrigerators
Development Status of High-Thrust Density Electrostatic Engines
Development Status of the NASA 30-cm Ion Thruster and Power Processor
Die Systematik der Kombinationsantriebe in der Luft- und Raumfahrt
Dimensional Variations in DLBMM of Aerospace Alloys
Discoverer Program Performance Analysis Report. Flight of FTV-1029. 13 August 1959 (30-Day Report)
Dissipation in Metal Welded Bellows and Its Consequences for Sub-Kelvin Refrigerators
Double Vortex Tube as Heat Exchanger and Flow Impedance for a Pulse Tube Refrigerator
Dry Laser Beam Micro-milling (DLBMM) of Aerospace Alloys
Ductile, High Heat Capacity, Magnetic Regenerator Alloys for the 10 to 80 K Temperature Range
Dynamik der Glieder des Speiseteils im Pneumatiksystem eines Schleppers
Effects of Spacecraft Interference on a 136 M Hz PCM Telemetry Data Link