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Wind Tunnel Investigation Of Thermal And Pressure Environments In The Base Of The Saturn S Ic Booster From Mach 01 To 35
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Book Synopsis Wind-tunnel Investigation of Thermal and Pressure Environments in the Base of the Saturn S-IC Booster from Mach 0.1 to 3.5 by : Robert A. Wasko
Download or read book Wind-tunnel Investigation of Thermal and Pressure Environments in the Base of the Saturn S-IC Booster from Mach 0.1 to 3.5 written by Robert A. Wasko and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of Thermal and Pressure Environments in the Base of the Saturn S-IC Booster from Mach 0.1 to 3.5 by : Robert A. Wasko
Download or read book Wind-tunnel Investigation of Thermal and Pressure Environments in the Base of the Saturn S-IC Booster from Mach 0.1 to 3.5 written by Robert A. Wasko and published by . This book was released on 1966 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1966 with total page 1470 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of Base Heating on a 5.47-per-cent Scale Model of the Saturn S-1 Booster at Transonic Mach Numbers by : T. L. Kennedy
Download or read book An Investigation of Base Heating on a 5.47-per-cent Scale Model of the Saturn S-1 Booster at Transonic Mach Numbers written by T. L. Kennedy and published by . This book was released on 1961 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the 16-ft transonic tunnel of the propulsion wind tunnel facility at the Arnold Center to evaluate base heating of the Saturn S-1 booster. Various turbine exhaust stack configurations were tested over a Mach number range of 0.6 to 1.5, an altitude range of 10,000 ft to 42,000 ft, and a missile angle-of-attack range of 0 to -7 1/2 deg. Rocket engines using liquid oxygen and RP-1 were used to simulate the full-scale engine exhaust, and hydrogen was used to simulate the turbo-pump exhaust. Base burning at all test conditions was eliminated for only one of the turbine exhaust stack configurations. Various degrees of base burning were obtained for all other exhaust stack configurations, but no burning occurred at a free-stream Mach number of 1.5 for the trajectory altitude. At altitudes above 29,000 ft, only localized base burning occurred and the accompanying heating rates were low.
Book Synopsis Wind-tunnel Investigation of the Aerodynamic Pressures on the Apollo Launch Escape Vehicle Configuration by : William C. Moseley (Jr.)
Download or read book Wind-tunnel Investigation of the Aerodynamic Pressures on the Apollo Launch Escape Vehicle Configuration written by William C. Moseley (Jr.) and published by . This book was released on 1970 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 0.30 to 1.20 of the Static Aerodynamic Characteristics of a Two-stage Saturn Launch Vehicle by :
Download or read book Wind-tunnel Investigation at Mach Numbers from 0.30 to 1.20 of the Static Aerodynamic Characteristics of a Two-stage Saturn Launch Vehicle written by and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Aerodynamic Pressures on the Apollo Command Module Configuration by : William C. Moseley
Download or read book Wind-tunnel Investigation of the Aerodynamic Pressures on the Apollo Command Module Configuration written by William C. Moseley and published by . This book was released on 1969 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind tunnel study of aerodynamic pressures on Apollo command module configuration.
Book Synopsis Transonic Wind-tunnel Investigation of the Aerodynamics Characteristics of Various Saturn 5 Configurations by :
Download or read book Transonic Wind-tunnel Investigation of the Aerodynamics Characteristics of Various Saturn 5 Configurations written by and published by . This book was released on 1964 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of Saturn S-IC AERODYNAMIC Engine Gimbal Forces and Base Pressures Using a Cold-flow-jet Simulation Technique by : Bernard J. Blaha
Download or read book Wind-tunnel Investigation of Saturn S-IC AERODYNAMIC Engine Gimbal Forces and Base Pressures Using a Cold-flow-jet Simulation Technique written by Bernard J. Blaha and published by . This book was released on 1967 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 0.40 to 1.20 of the Static Aerodynamic and Control Characteristics of a Model of a Nonlifting Reeintry Capsule in Combination with a Rocket Booster by : Albin O. Pearson
Download or read book Wind-tunnel Investigation at Mach Numbers from 0.40 to 1.20 of the Static Aerodynamic and Control Characteristics of a Model of a Nonlifting Reeintry Capsule in Combination with a Rocket Booster written by Albin O. Pearson and published by . This book was released on 1960 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 by : Dennis E. Fuller
Download or read book Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 written by Dennis E. Fuller and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Base Heat Transfer, Pressure Ratios, and Configuration Effects Obtained on a 1/27 Scall Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 by : John L. Allen
Download or read book Base Heat Transfer, Pressure Ratios, and Configuration Effects Obtained on a 1/27 Scall Saturn (C-1) Model at Mach Numbers from 0.1 to 2.0 written by John L. Allen and published by . This book was released on 1963 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Large-scale Wind-tunnel Investigation of an M1-L Lifting Body with an Inflatable and a Rigid Afterbody by : Kenneth W. Mort
Download or read book Large-scale Wind-tunnel Investigation of an M1-L Lifting Body with an Inflatable and a Rigid Afterbody written by Kenneth W. Mort and published by . This book was released on 1969 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation at Transonic Speeds of the Static Aerodynamic Characteristics and Pressure Distributions of a Three-stage Saturn Launch Vehicle by :
Download or read book Wind Tunnel Investigation at Transonic Speeds of the Static Aerodynamic Characteristics and Pressure Distributions of a Three-stage Saturn Launch Vehicle written by and published by . This book was released on 1963 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cryogenic Wind Tunnels: A Comprehensive, Annotated Bibliography by : Marie H. Tuttle
Download or read book Cryogenic Wind Tunnels: A Comprehensive, Annotated Bibliography written by Marie H. Tuttle and published by . This book was released on 1991 with total page 146 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Langley Hotshot Tunnel Operations with Helium at Mach Numbers in Excess of 30 by : Charles George Miller
Download or read book Langley Hotshot Tunnel Operations with Helium at Mach Numbers in Excess of 30 written by Charles George Miller and published by . This book was released on 1970 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The High-speed Flexible-throat Supersonic Wind Tunnel by :
Download or read book The High-speed Flexible-throat Supersonic Wind Tunnel written by and published by . This book was released on 1948 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
