Acceleration of Particles with Interaction Between High-Frequency Fields and a Plasma
Advanced Components for Cryogenic Integration
Advanced Cryogenic Integration and Cooling Technology for Space-Based Long Term Cryogen Storage
Air Transport versus High-Speed Rail: From Physics to Economics
Antimatter Production for Near-Term Propulsion Applications
Antimatter propulsion, status and prospects
Apparatus for Obtaining Isotropic Radiation of a Film Emulsion Patent Application
Approximate formulas for Franck-Condon factors
A program to measure new energetic particle nuclear interaction cross sections
Assessment of the advantages and feasibility of a nuclear rocket for a manned Mars mission
A thermalized ion explosion model for high energy sputtering and track registration
ATOMIC OXYGEN DURABILITY EVALUATION OF A UV CURABLE CERAMER PROTECTIVE COATING
Comments on a paper by Katz regarding charge exchange models
Comparison of ARTEMIS Data with the Lunar Plasma Design Environment for NASA Crewed Missions
Concepts for the design of an antimatter annihilation rocket
Development of Improved Sealed Ag- Zn Battery for Mariner 1969, Part 1, 6 November 1967 - 3 May 1968
Diagnostic of a Nonequilibrium Plasma for Mhd Generators
Effects of Neutral Gas Release on Current Collection During the Charge-2 Rocket Experiment
Environmental Interactions Technology Status
Evaluation of the space disposal of defense nuclear waste, Phase 2. Volume 1: Executive summary
Evaluation of the space disposal of defense nuclear waste, phase 2. Volume 2: Technical Report
Final Qualification and Early On-Orbit Performance of the RHESSI Cryocooler
Focus Control System for Solar Thermal Propulsion
Fusion energy for space missions in the 21st Century
Fusion energy for space missions in the 21st century: Executive summary
Galactic cosmic ray transport methods: Past, present and future
GROUND SIMULATION OF HYPERVELOCITY SPACE DEBRIS IMPACTS ON POLYMERS
High-Altitude Pressure Measurement in the Orbital Re-Entry Experiment (OREX)
High Current Beam Emissions from Spacecraft
How Will Sunsat Power Be Captured on Earth?
Initial results of SEPAC scientific achievement
Investigation ff Advanced High Energy Space Storable Propellant System
Ion engine propelled Earth-Mars cycler with nuclear thermal propelled transfer vehicle, volume 2
JPRS Report: Science and Technology, Central Eurasia: Engineering and Equipment
Laser Ablation of Solid Materials, Laser Ablation Propulsion
Launch vehicle integration requirements for SP-100