WebApr 21, 2016 · Four space shuttle wing leading edge concepts. ... Preliminary thermal/structural analysis of a carbon/carbon refractory-metal heat-pipe-cooled wing leading edge. In: Thornton, EA (ed.) Thermal structures and materials for high-speed flight (Progress in Astronautics and Aeronautics) ... WebSep 5, 2014 · Four space shuttle wing leading edge concepts J. Spacecraft Rockets (1974) C.J. Camarda Analysis and Radiant Heating Tests of a Heat-pipe-cooled Leading Edge (1977) C.J. Camarda Application of Formal Optimization Techniques in Thermal/structural Design of a Heat-pipe-cooled Panel for a Hypersonic Vehicle (1987)
Heat transfer characteristics and limitations analysis of heat …
WebA heat-pipe-cooled Space Shuttle orbiter wing leading edge was compared and evaluated against three alternate leading edge candidates: a refurbishable ablative design, and two … WebFeb 6, 2024 · To achieve high-speed flight, hypersonic vehicles will choose sharp structures in the stationary point areas such as spiked blunt-body and wing leading edge of vehicles. The aerodynamic heating in these areas is more intense than that in other region, so these stationary point areas become the key position of hypersonic vehicle heat protection. cycads for pleasure newcastle
The Leading Edge NASA
WebMcDonnell Douglas Astronautics Co. (MDAC) compared four space shuttle wing leading-edge concepts: a passive carbon-carbon concept, a passive coated-columbium concept, an ... shuttle-type heat-pipe-cooled leading edge to … WebJun 21, 1993 · The Leading Edge. A close-up view of the exterior of space shuttle Endeavour's crew cabin, starboard wing and payload bay door was provided by the … WebSpace Shuttle Discovery as it approaches the International Space Station during the STS-114 on 28 July 2005. The Space Shuttle thermal protection system (TPS) is the barrier that protected the Space Shuttle Orbiter during the searing 1,650 °C (3,000 °F) heat of atmospheric reentry. cycads design minecraft