[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

KO et al., 1981 - Google Patents

Preflight reentry heat transfer analysis of Space Shuttle

KO et al., 1981

Document ID
4732738651802664387
Author
KO W
QUINN R
Gong L
SCHUSTER L
Gonzales D
Publication year
Publication venue
1st Flight Test Conference

External Links

Snippet

A SPAR (structural performance and resizing) finitc clcment thermal analysis computer program was used in the reentry heat transfer analysis of the space shuttlc. One typical wing cross section and a midfuse-. lagc cross section wcre selcctcd for the analysis, The surface …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/52—Protection, safety or emergency devices; Survival aids
    • B64G1/58—Thermal protection, e.g. heat shields
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/38—Constructions adapted to reduce effects of aerodynamic or other external heating
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/40—Sound or heat insulation, e.g. using insulation blankets

Similar Documents

Publication Publication Date Title
Bisplinghoff Some structural and aeroelastic considerations of high-speed flight the nineteenth wright brothers lecture
Ko et al. Finite-element reentry heat-transfer analysis of space shuttle orbiter
Bolender et al. Modeling unsteady heating effects on the structural dynamics of a hypersonic vehicle
Blosser et al. Reusable metallic thermal protection systems development
KO et al. Preflight reentry heat transfer analysis of Space Shuttle
Monti et al. Thermal shielding of a reentry vehicle by ultra-high-tempreature ceramic materials
Gong et al. Thermal response of space shuttle wing during reentry heating
Kontinos et al. Numerical simulation of metallic thermal protection system panel bowing
Ko et al. Reentry thermal analysis of a generic crew exploration vehicle structure
Gong et al. Reentry heating analysis of space shuttle with comparison of flight data
Thompson et al. Hypersonic boundary layer transition for X-33 phase II vehicle
Ko Solution accuracies of finite element reentry heat transfer and thermal stress analyses of space shuttle orbiter
Gong et al. Comparison of flight-measured and calculated temperatures on the space shuttle orbiter
Blosser et al. Wing leading-edge design concepts for airbreathing hypersonic waveriders
Polesky et al. Three-dimensional thermal structural analysis of a swept cowl leading edge subjected to skewed shock-shock interference heating
Smith et al. An investigation of gap heating due to stepped tiles in zero pressure gradient regions of the shuttle orbiter thermal protection system
Ko et al. Thermal stress analysis of space shuttle orbiter subjected to reentry aerodynamic heating
Cunningham et al. Space shuttle wing leading edge heating environment prediction derived from development flight data
Wood et al. Comparison of CFD predictions with shuttle global flight thermal imagery and discrete surface measurements
LEE et al. Aerothermodynamic entry environment of the Space Shuttle Orbiter
Schuh Transient Temperature Distributions and Thermal Stresses in a Skin-Shear Web Configuration at High-Speed Flight for a Wide Range of Parameters
Neumann et al. Aerodynamic heating to the hypersonic research aircraft, X-24C
WILLIAMS et al. An assessment of the Space Shuttle Orbiter thermal environment usingflight data
Newell A study of thermo-structural design concepts for lifting entry vehicles
Wood et al. Assessment of CFD hypersonic turbulent heating rates for space shuttle orbiter