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Book Aerothermal Performance of a Radiatively and Actively Cooled Panel at Mach 6 6

Download or read book Aerothermal Performance of a Radiatively and Actively Cooled Panel at Mach 6 6 written by Charles P. Shore and published by . This book was released on 1979 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerothermal Performance of a Radiatively and Actively Cooled Panel at Mach 66

Download or read book Aerothermal Performance of a Radiatively and Actively Cooled Panel at Mach 66 written by and published by . This book was released on 1979 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flight-weight radiative and actively cooled honeycomb sandwich panel (RACP was subjected to multiple cycles of both radiant and aerothermal heating. The 0.61-m (2 ft) by 1.22-m (4 ft) test specimen incorporated essential features of a full-scale 0.61-m (2 ft) by 6.10-m (20 ft) RACP designed to withstand a heat flux of 136 kW/m2 (12 Btu/sq. ft-sec). The panel consisted of Rene 41 heat shields, a thin layer of high-temperature insulation, and an aluminum honeycomb sandwich panel with coolant tubes next to the sandwich skin. A 60/40 mass solution of ethylene glycol/water was used to cool the panel which successfully withstood a total of 3.5 hr of radiant heating and 137 sec exposure to an M = 6.6 test stream. Heatshield temperatures reached 1080 K (1945 R), and cooled-panel temperatures reached 382 K (687 R) midway between coolant tubes. Simulation of the full-scale panel indicated that the full-scale RACP would perform as expected. The tests revealed no evidence of coolant leadkage or hot- gas ingress which would seriously degrade the RACP performance. (Author).

Book Aerothermal Performance of a Radiatively and Actively Cooled Panel at Mach 6 6

Download or read book Aerothermal Performance of a Radiatively and Actively Cooled Panel at Mach 6 6 written by Charles P. Shore and published by . This book was released on 1979 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Conference Publication

Download or read book NASA Conference Publication written by and published by . This book was released on 1992 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Current Technology for Thermal Protection Systems

Download or read book Current Technology for Thermal Protection Systems written by and published by . This book was released on 1992 with total page 336 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summarizes the history and operational experience of thermal protection systems utilized in the national space program, and also covers development efforts in thermal insulation, refractory materials and coatings, actively cooled structures, and two-phase thermal control systems.

Book NASA Technical Paper

Download or read book NASA Technical Paper written by and published by . This book was released on 1982 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Flightweight Radiantly and Actively Cooled Panel

Download or read book Flightweight Radiantly and Actively Cooled Panel written by Charles P. Shore and published by . This book was released on 1982 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Flightweight Radiantly and Actively Cooled Panel

Download or read book Flightweight Radiantly and Actively Cooled Panel written by Charles P. Shore and published by . This book was released on 1982 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by and published by . This book was released on 1980 with total page 232 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Scientific and Technical Publications

Download or read book NASA Scientific and Technical Publications written by and published by . This book was released on 1987 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Evaluation of Active Cooling Systems for a Mach 6 Hypersonic Transport Airframe

Download or read book Evaluation of Active Cooling Systems for a Mach 6 Hypersonic Transport Airframe written by R. G. Helenbrook and published by . This book was released on 1971 with total page 924 pages. Available in PDF, EPUB and Kindle. Book excerpt: Transpiration and convective cooling concepts are examined for the fuselage and tail surface of a Mach 6 hypersonic transport aircraft. Hydrogen, helium, and water are considered as coolants. Heat shields and radiation barriers are examined to reduce heat flow to the cooled structures. The weight and insulation requirements for the cryogenic fuel tanks are examined so that realistic totals can be estimated for the complete fuselage and tail. Structural temperatures are varied to allow comparison of aluminum alloy, titanium alloy, and superalloy construction materials. The results of the study are combined with results obtained on the wing structure, obtained in a previous study, to estimate weights for the complete airframe. The concepts are compared among themselves, and with the uncooled concept on the basis of structural weight, cooling system weight, and coolant weight.

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1987 with total page 1126 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Book Design of a Convective Cooling System for a Mach 6 Hypersonic Transport Airframe

Download or read book Design of a Convective Cooling System for a Mach 6 Hypersonic Transport Airframe written by R. G. Helenbrook and published by . This book was released on 1971 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of analytical and design studies are presented for a water-glycol convective cooling system for the airframe structure of a hypersonic transport. System configurations and weights are compared. The influences of system pressure drop and flow control schedules on system weight are defined.

Book Design and Fabrication of a Radiative Actively Cooled Honeycomb Sandwich Structural Panel for a Hypersonic Aircraft

Download or read book Design and Fabrication of a Radiative Actively Cooled Honeycomb Sandwich Structural Panel for a Hypersonic Aircraft written by D. A. Ellis and published by . This book was released on 1978 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Monthly Catalogue  United States Public Documents

Download or read book Monthly Catalogue United States Public Documents written by and published by . This book was released on 1983 with total page 1050 pages. Available in PDF, EPUB and Kindle. Book excerpt: