24 AUTO-TRACTOR FUEL SYSTEM FOR LNG
231 DEVELOPMENT OF THE HTS MAGNET FOR THE SUPERCONDUCTING MAGLEV - PROJECT OVERVIEW
ac Breakdown Properties and Solidification States of Solidified Alcohol Aqueous Solutions
Achieving Supportability on Exploration Missions with In-Space Servicing
A Comparison Study between Conventional and Cryogenic Machining
Acquisition/Expulsion System for Earth Orbital Propulsion System Study. Volume 1: Summary Report
Acquisition/Expulsion System for Earth Orbital Propulsion System Study. Volume 2: Cryogenic Design
A cryogenic electric propulsion system in cargo vessels
Active Control of Cryogenic Propellants in Space
Active Costorage of Cryogenic Propellants for Exploration
Adaptive Structures Flight Experiments
Advanced Ceramics for Use as Fuel Element Materials in Nuclear Thermal Propulsion Systems
Advanced Chemical Propellants: The High Energy Density Matter Program
Advanced Chemical Propulsion Study
Advanced Cryogenic Integration and Cooling Technology for Space-Based Long Term Cryogen Storage
Advanced Cryogenic Rocket Engine Program, Aerospike Nozzle Concept
Advanced Cryogenic Rocket Engine Program, Aerospike Nozzle Concept. Volume 1
Advanced Cryogenic Solid Hybrid Rocket Engine Developments: Concept and Test Results
Advanced Injector Concepts Investigation Final Summary Report
Advanced Oxygen-Hydrocarbon Rocket Engine Study
Advanced pressurization systems for cryogenic propellants Final report, 20 Nov. 1963 - 25 Jun. 1965
Advanced Space-Based Detector Research at the Air Force Research Laboratory (PREPRINT)
Advanced space transportation systems, BARGOUZIN booster
Advanced studies on multi-layer insulation systems Final report
Advancements in Low Leakage Valves for Long Duration Missions
Aeroacoustic Measurements of a Scaled Half-Model at High Reynolds Numbers
Aeroelastic Scaling of a High-Aspect-Ratio Wing Incorporating a Semi-Aeroelastic Hinge
After Math - Foamology and Flight Rationale
A hybrid engine concept for multi-fuel blended wing body
Air Force Research Laboratory Cryocooler Technology Development
Air Force Research Laboratory Space Cryogenic Technology Research Initiatives
Air Force Reusable Rocket Engine Program XLR129-P-1. Volume II
Air Force Reusable Rocket Engine Program XLR129-P-1. Volume III
Alternative Fuel in Transport Aviation and Estimation of Its Application Efficiency
Ammonia Analysis by Gas Chromatography/Infrared Detector (CG/IRD)
Analysis and Test of Low Profile Aluminum Aerospace Tank Dome
Analysis of Conformable Pressure Vessels: Introducing the Multi-Bubble
Analysis of low-thrust liquid rocket engines with a methane air pump unit