Aerodynamic characteristics of a booster and an ascent shuttle configuration from Mach 0.28 to Mach 10.4
Wind tunnel tests to determine aerodynamic characteristics of booster and ascent shuttle configuration from Mach 0.28 to 10.4
Bernot, P. T.↗
SEARCH · Search NASA
Results for “Booster”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Shock interference heating on the space shuttle booster during ascent
Aerothermodynamic shock heating of space shuttle booster surface during atmospheric ascent
Brevig, O.↗
Flight dynamics of a straight wing space shuttle booster during entry
Dynamic flight control simulation for straight wing space shuttle booster entry
Kimbrel, L. G.↗
Booster wing geometry trade studies
Booster wing geometry effects on space shuttle design requirements
Butsko, J. E.↗
Booster thermal protection system evaluation
Launch vehicle thermal protection system evaluation based on thermal and pressure distributions over exposed booster surface
Norton, A. M.↗
The heat sink concept for the space shuttle booster
Cost and weight data for space shuttle booster heat sink structural concept
Prunty, J.↗
Technology for low cost solid rocket boosters
Technology development for low cost rocket boosters and estimates of total cost reduction obtainable by implementation
Ciepluch, C.↗
Space shuttle: Aerodynamic forces and moment on orbiter and booster during space shuttle abort separation
Aerodynamic forces and moments on orbiter and booster during space shuttle abort separation
De Bevoise, J. M.↗
Space shuttle: Low speed aerodynamic characteristics of the McDonnell Douglas space shuttle booster. Douglas Long Beach, low speed, wind tunnel test results
Low speed aerodynamic characteristics of McDonnell Douglas scale model space shuttle booster
Finch, C. M.↗
Space shuttle: Longitudinal aerodynamic characteristics of the GD/Convair B8B booster. Wind tunnel test results
Transonic wind tunnel tests of longitudinal aerodynamic characteristics of GD/Convair B8B space shuttle booster model
Carter, W. V.↗
Space shuttle: Longitudinal and lateral aerodynamic characteristics of the Convair B8B space shuttle booster with modifications
Hypervelocity wind tunnel tests of Convair B8B space shuttle booster and model configuration perturbations
Robinson, H.↗
Space shuttle: Static stability and control investigation of the NAR-GDVC straight wing booster (B-8H modified) with the straight wing orbiter (130G) or delta wing orbiter (134B)
Trisonic wind tunnel tests on static stability and controllability of NAR/GD space shuttle and booster
Allen, E. C.↗
Space Shuttle: MDAC/MMC space shuttle booster determination of stability and control characteristics and power effects at subsonic speed, Mach numbers zero and 0.26
Low speed wind tunnel tests of stability and control characteristics of space shuttle booster at subsonic speeds
Michna, D.↗
Space shuttle: Determination of static longitudinal and lateral directional stability characteristics of the NR/GD delta wing Orbiter/Saturn 5 S-IC booster
Wind tunnel tests on longitudinal and lateral directional stability of NAR/GD delta wing orbiter mated to Saturn 5 S-1C booster
Muhlhauser, C. H.↗
Space shuttle: M/DAC delta wing booster; determination of low speed directional stability characteristics
Low speed wind tunnel tests of directional stability characteristics for M/DAC delta wing booster
Finch, C. M.↗
Space Shuttle: Subsonic Aerodynamic Characteristics of MDAC/MMC Space Shuttle Booster Configuration at Mach Number 0.26
Subsonic aerodynamic characteristics of MDAC/MMC space shuttle booster configuration at Mach 0.26
Michna, D.↗
Aerodynamic heating of a space shuttle delta-wing booster at free stream Mach 7.4
Aerodynamic heating of space shuttle delta-wing booster at free Mach stream 7.4
Derose, C. E.↗
Space shuttle: Static aerodynamic characteristics of the Boeing space shuttle booster configuration at Mach 0.10 to 0.29
Wind tunnel tests to determine static aerodynamic characteristics of space shuttle booster configuration at subsonic speeds
Houser, J.↗