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Challenges of Designing a Passive Thermal Control System for the Astrobotic Peregrine Lunar Lander
Streamlined Approach to Spatial Mapping of Complex 3D Thermal Boundary Condition Data
Selecting Thermal Designs Cosmic Background Explorer Spacecraft and Instruments
Buckling and Steady Flutter of Heat-Compressed Panels in a Supersonic Flow
Mission Definition Study for Stanford Relativity Satellite. Volume 3 Appendices
Thermal Testing of a Stacked Core Mirror for UV Applications
The Thermal Degradation of Perfluoropolypyridine
Research and Development in the Field of High Altitude Plastic Balloons
Thermal Fluid Analysis for Nuclear Thermal Propulsion Radiation Shield
The Variation of Heating Rates in a 1/30 Scale Booster Rocket Exhaust Jet
Structural Design for Aerodynamic Heating. Part II. Analytical Studies
Solar Simulation for the CREST Preflight Thermal-Vacuum Test at B-2
Physics of Colloids in Space--Plus (PCS+) Experiment Completed Flight Acceptance Testing
Orbital Thermal Analysis of Lattice Structured Spacecraft Using Color Video Display Techniques
Beryllium Fabrication Methods Development Program - Thermal Treatment
Low Enriched Uranium (LEU) Nuclear Thermal Propulsion: System Overview and Ground Test Strategy
Ares V an Enabling Capability for Future Space Astrophysics Missions
Compositional Ground Truth of Diviner Lunar Radiometer Observations
Aeroheating Thermal Analysis Methods for Aerobraking Mars Missions
Large Astronomical Satellite Platform Arrangement
Laser Holographic Nondestructive Testing of the NASA X-248 Rocket Motor
Lunar Return Reentry Thermal Analysis of a Generic Crew Exploration Vehicle Wall Structures
LDEF Thermal Control Coatings Post-Flight Analysis
Mars Ascent Vehicle Flight Analysis
Mars Sample Return Using Commercial Capabilities: Mission Architecture Overview
Mars Sample Return Using Commercial Capabilities: Mission Architecture Overview
Design and Development of a Lunar Radiometer
Compact, Passively Q-Switched Nd: YAG Laser for the MESSENGER Mission to the Planet Mercury
Investigation of CS Sub 2 O-Photocathodes (Type S 1) Final Technical Report, Mar. 1967 - Feb. 1968
Multi-Scale Modeling of Low-Density Carbon-Phenolic Ablators
Thermal Analysis of the Spacelab Mission D2 Utility Support Structure and Its Payloads
HST Solar Generator Electrical Performance During the First Year in Orbit
The Average Temperature Errors of a Satellite in a Space Chamber Due to Environmental Imperfections
AFE (Aeroassisted Flight Experiment) Ion Mass Spectrometer Design Study