Synonyme wurden verwendet für:
Reentry
•
shielding
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keywords:(Reentry shielding)
TPS Architectures and the Influence of Material and Architecture on Failure Mode Evolution
SOME CONSIDERATIONS OF THE PERFORMANCE OF A MANEUVERABLE, LIFTING-BODY, ENTRY VEHICLE
Advanced Entry Systems Concepts
Space Shuttle Columbia Accident Investigation: Forensic Tools, Techniques, and Results
Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Mission Applications Study
Micrometeoroid and Orbital Debris (MMOD) Risk Overview
Design of Orbital Re-Entry Experiment Vehicle and Outline of the Experiment
Multiwall Thermal Protection System Engineering Aspects
Evaluation of the NASA Arc Jet Capabilities to Support Mission Requirements
Residual Mechanical Properties of Ti-6Al-4V after Simulated Space Shuttle Reentry
Space Tug Aerobraking Study. Volume 1 Executive Summary
Thermal-Structural Evaluation of Td Ni-20CR Thermal Protection System Panels
Regolith Derived Heat Shield for Planetary Body Entry and Descent System with In Situ Fabrication
Apollo IV (AS-501): Convective Heating Predictions of Flight Data
Development of 3D Woven Ablative Thermal Protection Systems (TPS) for NASA Spacecraft
Orion Flight Test-1 Thermal Protection System Instrumentation
Thermal Control Materials on MISSE-6 with Comparison to Earlier Flight Data
A Pyrotechnic-Activated Calorimeter for Flight Research at Lunar Return Velocity
A Pyrotechnic-Activated Calorimeter for Flight Research at Lunar Return Velocity
Measurements of Vehicle Glow on the Space Shuttle
Design and Fabrication of Metallic Thermal Protection Systems for Aerospace Vehicles
Shuttle/Agena Study. Annex C Space Shuttle Candidate Insulator/Propellant
Preliminary Study of a Reentry Body Etude Preliminaire d'UN Corps de Rentree
Is the Sky Really Falling? An Overview of Orbital Debris
Sharp Technologies as Applied to a Crew Transfer Vehicle
Study of Heat Shielding Requirements for Manned MARS Landing and Return Missions Summary Report
Launch of Second Experiment in Project FIRE
Lunar Return Reentry Thermal Analysis of a Generic Crew Exploration Vehicle Wall Structures
APOLLO Ablator Thermal Performance at Superorbital Entry Velocities
Emergency Earth Orbital Escape Device Patent Application
Payload Performance Analysis for a Reusable Two-Stage-to-Orbit Vehicle
Manned Space Flight Nuclear System Safety. Volume 1. Base Nuclear System Safety. Final Report
Results of Tests on a Specimen of the SRB Aft Skirt Heat Shield Curtain in the MSFC LRLF
Debris/Ice/TPS Assessment and Photographic Analysis for Shuttle Mission STS-28R