TA1: Launch Propulsion Systems 1.6 Balloon Launch Systems - Follow-Up
No abstract available
Fairbrother, Debora↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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An Empirical Non-TNT Approach to Launch Vehicle Explosion Modeling
No abstract available
Blackwood, James M.↗
New Developments in ISHM for NASA Ground, Launch, and Flight Systems
No abstract available
Figueroa, Fernando↗
GPM Product Evaluations, Algorithms, and Processes: GV in the Post-Launch and Extended Mission
No abstract available
Precipitation↗
Essential Failure Modes and Effects Analysis (FMEA) and the Design Influence of Space Launch Vehicle Avionics Systems
No abstract available
Al Hassan, Mohammad↗
Analyses of Kennedy Space Center Tropospheric Doppler Radar Wind Profiler Data for Space Launch System Program Certification
No abstract available
Barbre, Robert E., Jr.↗
The Implementation of Maximum Likelihood Estimation in Space Launch System Vehicle Design
No abstract available
Thompson, S. B.↗
Flame Speed Sensitivities for Modeling Launch Vehicle Explosion Risk
No abstract available
Coates, Ashley↗
Space shuttle phase B wind tunnel model and test information. Volume 3: Launch configuration
Archived wind tunnel data are available for flyback booster or other alternative recoverable configurations as well as reusable orbiters studied during initial development (Phase B) of the Space Shuttle. Considerable wind tunnel data was acquired by the competing contractors and the NASA Centers for an extensive variety of configurations with an array of wing and body planforms. All contractor and NASA wind tunnel data acquired in the Phase B development have been compiled into a data base and are available for application to current winged flyback or recoverable booster aerodynamic studies. The Space Shuttle Phase B Wind Tunnel Database is structured by vehicle component and configuration type. Basic components include booster, orbiter and launch vehicle. Booster configuration types include straight and delta wings, canard, cylindrical, retroglide and twin body. Orbital configuration types include straight and delta wings, lifting body, drop tanks and double delta wings. This is Volume 3 (Part 2) of the report -- Launch Configuration -- which includes booster and orbiter components in various stacked and tandem combinations.
Glynn, J. L.↗