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Pressure Distributions On A 002 Scale Space Shuttle Orbiter Nose At Mach 215 In Helium
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Book Synopsis Pressure Distributions on a 0.02-scale Space Shuttle Orbiter Nose at Mach 21.5 in Helium by : George C. Ashby (Jr.)
Download or read book Pressure Distributions on a 0.02-scale Space Shuttle Orbiter Nose at Mach 21.5 in Helium written by George C. Ashby (Jr.) and published by . This book was released on 1994 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722698805 Total Pages :78 pages Book Rating :4.6/5 (988 download)
Book Synopsis Pressure Distributions on a 0. 02-Scale Space Shuttle Orbiter Nose at Mach 21. 5 in Helium by : National Aeronautics and Space Administration (NASA)
Download or read book Pressure Distributions on a 0. 02-Scale Space Shuttle Orbiter Nose at Mach 21. 5 in Helium written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-10 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure distributions on a 0.02-scale model of the Space Shuttle orbiter forward fuselage were obtained in the 22-inch aerodynamic leg of the Langley Hypersonic Helium Tunnel Facility at a nominal free-stream Mach number of 21.5 and a ratio of specific heats of 1.67 for inclusion in the database of the Shuttle entry air data system (SEADS). The data were measured at model angles of attack of 0 deg to 50 deg in 5 deg increments for zero sideslip angle and at model sideslip angles of -5 deg to 5 deg for angles of attack equal to 5, 20, 35, and 40 deg. These data displayed trends similar to those observed in other wind tunnels at Mach 6 and 10 in air. Specifically noted is a shift in the location of the stagnation point at angles of attack above 15 deg; this effect did not, however, occur in flight. By comparison, the data obtained at Mach 6 in the Langley Hypersonic CF4 Tunnel, corresponding to a lower ratio of specific heats in the postshock region than those in helium and air, showed some reduction of the stagnation point shift at the higher angles of attack. The differences between flight and wind tunnel pressure distributions are believed due primarily to high-temperature gas chemistry effects in flight, which include lower effective specific heat ratios but which were not completely duplicated in the wind tunnels. Ashby, George C., Jr. and Bernot, Peter T. and Woods, William C. Langley Research Center...
Book Synopsis Pressure Distributions on a 0.02-scale Space Shuttle Orbiter Nose at Mach 21.5 in Helium by : George C. Ashby
Download or read book Pressure Distributions on a 0.02-scale Space Shuttle Orbiter Nose at Mach 21.5 in Helium written by George C. Ashby and published by . This book was released on 1994 with total page 73 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Comparison of Predicted and Experimental Real-gas Pressure Distributions on Space Shuttle Orbiter Nose for Shuttle Entry Air Data System by : Judy L. Shinn
Download or read book Comparison of Predicted and Experimental Real-gas Pressure Distributions on Space Shuttle Orbiter Nose for Shuttle Entry Air Data System written by Judy L. Shinn and published by . This book was released on 1980 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Distributions Obtained on a 0.04-scale and 0.02-scale Model of the Space Shuttle Orbiter's Forward Fuselage in the Langley 20-inch Mach 6 Air Tunnel by :
Download or read book Pressure Distributions Obtained on a 0.04-scale and 0.02-scale Model of the Space Shuttle Orbiter's Forward Fuselage in the Langley 20-inch Mach 6 Air Tunnel written by and published by . This book was released on 1983 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flow-field Surveys on the Windward Side of the NASA 040A Space Shuttle Orbiter at 31 ̊angle of Attack and Mach 20 in Helium by : George C. Ashby
Download or read book Flow-field Surveys on the Windward Side of the NASA 040A Space Shuttle Orbiter at 31 ̊angle of Attack and Mach 20 in Helium written by George C. Ashby and published by . This book was released on 1977 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Distributions Obtained on a 0.04-scale and 0.02-scale Model of the Space Shuttle Orbiter's Forward Fuselage in the Langley Continuous Flow Hypersonic Tunnel by :
Download or read book Pressure Distributions Obtained on a 0.04-scale and 0.02-scale Model of the Space Shuttle Orbiter's Forward Fuselage in the Langley Continuous Flow Hypersonic Tunnel written by and published by . This book was released on 1983 with total page 68 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 1994 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Distributions Obtained on a 0.10-scale Model of the Space Shuttle Orbiter's Forebody in the Ames Unitary Plan Wind Tunnel by :
Download or read book Pressure Distributions Obtained on a 0.10-scale Model of the Space Shuttle Orbiter's Forebody in the Ames Unitary Plan Wind Tunnel written by and published by . This book was released on 1986 with total page 490 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Laminar Heat-transfer and Pressure-distribution Studies on a Series of Reentry Nose Shapes at a Mach Number of 19.4 in Helium by : RICHARD D. JR. WAGNER
Download or read book Laminar Heat-transfer and Pressure-distribution Studies on a Series of Reentry Nose Shapes at a Mach Number of 19.4 in Helium written by RICHARD D. JR. WAGNER and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted in the 2-in. helium tunnel at the Langley Research Center at a Mach number of 19.4 to determine the pressure distributions and heat-transfer characteristics of a family of reentry nose shapes. The pressure and heat-transfer-rate distributions on the nose shapes are compared with theoretical predictions to ascertain the limitations and validity of the theories at hypersonic speeds. The experimental results were found to be adequately predicted by existing theories. Two of the nose shapes were tested with variable-length flow-separation spikes. The results obtained by previous investigators of spike-nose bodies were found to prevail at the higher Mach number of the present investigation. (Author).
Book Synopsis Wind Tunnel Pressure Signatures for a 0.0041-scale Model of the Space Shuttle Orbiter by :
Download or read book Wind Tunnel Pressure Signatures for a 0.0041-scale Model of the Space Shuttle Orbiter written by and published by . This book was released on 1975 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flow-field Surveys on the Windward Side of the NASA 040A Space Shuttle Orbiter at 31 Ångle of Attack and Mach 20 in Helium by : George C. Ashby
Download or read book Flow-field Surveys on the Windward Side of the NASA 040A Space Shuttle Orbiter at 31 Ångle of Attack and Mach 20 in Helium written by George C. Ashby and published by . This book was released on 1977 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flow-field Surveys on the Windward Side of the NASA 040A Space Shuttle Orbiter at 31° Angle of Attack and Mach 20 in Helium by : George C. Ashby
Download or read book Flow-field Surveys on the Windward Side of the NASA 040A Space Shuttle Orbiter at 31° Angle of Attack and Mach 20 in Helium written by George C. Ashby and published by . This book was released on 1977 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Columbia Crew Survival Investigation Report by : Nasa
Download or read book Columbia Crew Survival Investigation Report written by Nasa and published by PDQ Press. This book was released on 2009 with total page 400 pages. Available in PDF, EPUB and Kindle. Book excerpt: NASA commissioned the Columbia Accident Investigation Board (CAIB) to conduct a thorough review of both the technical and the organizational causes of the loss of the Space Shuttle Columbia and her crew on February 1, 2003. The accident investigation that followed determined that a large piece of insulating foam from Columbia's external tank (ET) had come off during ascent and struck the leading edge of the left wing, causing critical damage. The damage was undetected during the mission. The Columbia accident was not survivable. After the Columbia Accident Investigation Board (CAIB) investigation regarding the cause of the accident was completed, further consideration produced the question of whether there were lessons to be learned about how to improve crew survival in the future. This investigation was performed with the belief that a comprehensive, respectful investigation could provide knowledge that can protect future crews in the worldwide community of human space flight. Additionally, in the course of the investigation, several areas of research were identified that could improve our understanding of both nominal space flight and future spacecraft accidents. This report is the first comprehensive, publicly available accident investigation report addressing crew survival for a human spacecraft mishap, and it provides key information for future crew survival investigations. The results of this investigation are intended to add meaning to the sacrifice of the crew's lives by making space flight safer for all future generations.
Book Synopsis Hypersonic and High Temperature Gas Dynamics by : John David Anderson
Download or read book Hypersonic and High Temperature Gas Dynamics written by John David Anderson and published by AIAA. This book was released on 1989 with total page 710 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.
Book Synopsis The Space Shuttle Decision by : T. A. Heppenheimer
Download or read book The Space Shuttle Decision written by T. A. Heppenheimer and published by . This book was released on 1999 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Long before the NASA was the throes of planning for the Apollo voyages to the Moon, many people had seen the need for a vehicle that could access space routinely. The idea of a reusable space shuttle dates at least to the theoretical rocketplane studies of the 1930s, but by the 1950s it had become an integral part of a master plan for space exploration. The goal of efficient access to space in a heavy-lift booster prompted NASA's commitment to the space shuttle as the vehicle to continue human space flight. By the mid-1960s, NASA engineers concluded that the necessary technology was within reach to enable the creation of a reusable winged space vehicle that could haul scientific and applications satellites of all types into orbit for all users. President Richard M. Nixon approved the effort to build the shuttle in 1972 and the first orbital flight took place in 1981. Although the development program was risky, a talented group of scientists and engineers worked to create this unique space vehicle and their efforts were largely successful. Since 1981, the various orbiters -Atlantis, Columbia, Discovery, Endeavour, and Challenger (lost in 1986 during the only Space Shuttle accident)- have made early 100 flights into space. Through 1998, the space shuttle has carried more than 800 major scientific and technological payloads into orbit and its astronaut crews have conducted more than 50 extravehicular activities, including repairing satellites and the initial building of the International Space Station. The shuttle remains the only vehicle in the world with the dual ability to deliver and return large payloads to and from orbit, and is also the world's most reliable launch system. The design, now almost three decades old, is still state-of-the-art in many areas, including computerized flight control, airframe design, electrical power systems, thermal protection system, and main engines. This significant new study of the decision to build the space shuttle explains the shuttle's origin and early development. In addition to internal NASA discussions, this work details the debates in the late 1960s and early 1970s among policymakers in Congress, the Air Force, and the Office of Management and Budget over the roles and technical designs of the shuttle. Examining the interplay of these organizations with sometimes conflicting goals, the author not only explains how the world's premier space launch vehicle came into being, but also how politics can interact with science, technology, national security, and economics in national government.
Download or read book Energiya-Buran written by Bart Hendrickx and published by Springer Science & Business Media. This book was released on 2007-12-05 with total page 541 pages. Available in PDF, EPUB and Kindle. Book excerpt: This absorbing book describes the long development of the Soviet space shuttle system, its infrastructure and the space agency’s plans to follow up the first historic unmanned mission. The book includes comparisons with the American shuttle system and offers accounts of the Soviet test pilots chosen for training to fly the system, and the operational, political and engineering problems that finally sealed the fate of Buran and ultimately of NASA’s Shuttle fleet.
