Rocket Drive For Long Range Bombers
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Rocket Drive For Long Range Bombers
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Author : Eugen Sanger
language : en
Publisher:
Release Date : 1952
Rocket Drive For Long Range Bombers written by Eugen Sanger and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with categories.
Rocket Drive For Long Range Bombers
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Author : E. Sänger
language : en
Publisher:
Release Date : 1944-01-01
Rocket Drive For Long Range Bombers written by E. Sänger and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1944-01-01 with categories.
A Rocket Drive For Long Range Bombers Ber Einen Raketenantrieb F R Fernbomber
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Author : Eugen Sänger
language : en
Publisher:
Release Date : 194?
A Rocket Drive For Long Range Bombers Ber Einen Raketenantrieb F R Fernbomber written by Eugen Sänger and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 194? with categories.
A Rocket Drive For Long Range Bombers
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Author : Eugen Sänger
language : en
Publisher:
Release Date : 1946
A Rocket Drive For Long Range Bombers written by Eugen Sänger and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1946 with Bombers categories.
The Hypersonic Revolution From Max Valier To Project Prime 1924 1967
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Author :
language : en
Publisher:
Release Date : 1998
The Hypersonic Revolution From Max Valier To Project Prime 1924 1967 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Aerodynamics, Hypersonic categories.
Dark Star
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Author : Matthew H. Hersch
language : en
Publisher: MIT Press
Release Date : 2023-12-26
Dark Star written by Matthew H. Hersch and has been published by MIT Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2023-12-26 with Technology & Engineering categories.
A captivating history of NASA’s Space Transportation System—the space shuttle—chronicling the inevitable failures of a doomed design. In Dark Star, Matthew Hersch challenges the existing narrative of the most significant human space program of the last 50 years, NASA’s space shuttle. He begins with the origins of the space shuttle: a century-long effort to develop a low-cost, reusable, rocket-powered airplane to militarize and commercialize space travel, which Hersch explains was built the wrong way, at the wrong time, and for all the wrong reasons. Describing the unique circumstances that led to the space shuttle’s creation by President Richard Nixon’s administration in 1972 and its subsequent flights from 1981 through 2011, Hersch illustrates how the space shuttle was doomed from the start. While most historians have accepted the view that the space shuttle’s fatal accidents—including the 1986 Challenger explosion—resulted from deficiencies in NASA’s management culture that lulled engineers into a false confidence in the craft, Dark Star reveals the widespread understanding that the shuttle was predestined for failure as a technology demonstrator. The vehicle was intended only to give the United States the appearance of a viable human spaceflight program until funds became available to eliminate its obvious flaws. Hersch’s work seeks to answer the perilous questions of technological choice that confront every generation, and it is a critical read for anyone interested in how we can create a better world through the things we build.
A Comparative Analysis Of The Performance Of Long Range Hypervelocity Vehicles
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Author : Alfred J. Eggers
language : en
Publisher:
Release Date : 1957
A Comparative Analysis Of The Performance Of Long Range Hypervelocity Vehicles written by Alfred J. Eggers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerodynamic heating categories.
The ballistic vehicle is found to be the least efficient of the several types studied in the sense that it generally requires the highest velocity at the end of powered flight in order to attain a given range. This disadvantage may be offset, however, by reducing convective heat transfer to the re-entry body through the artifice of increasing pressure drag in relation to friction drag - that is, by using a blunt body. Thus the kinetic energy required by the vehicle at the end of powered flight may be reduced by minimizing the mass of coolant material involved.
The Hypersonic Revolution
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Author : Richard Hallion
language : en
Publisher:
Release Date : 1987
The Hypersonic Revolution written by Richard Hallion and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with Aerodynamics, Hypersonic categories.
The Hypersonic Revolution From Max Valier To Project Prime 1924 1967
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Author : Richard Hallion
language : en
Publisher:
Release Date : 1987
The Hypersonic Revolution From Max Valier To Project Prime 1924 1967 written by Richard Hallion and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with Aerodynamics, Hypersonic categories.
The Subsonic Static Aerodynamic Characteristics Of An Airplane Model Having A Triangular Wing Of Aspect Ratio 3
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Author : Howard F. Savage
language : en
Publisher:
Release Date : 1957
The Subsonic Static Aerodynamic Characteristics Of An Airplane Model Having A Triangular Wing Of Aspect Ratio 3 written by Howard F. Savage and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerodynamics categories.
An investigation has been conducted to determine the effects of vertical-tail location and size on the subsonic aerodynamic characteristics of a model having a triangular wing. The wing had an aspect ratio of 3, an NACA 0003.5-63 section in the streamwise direction, and plain, trailing-edge ailerons. The wing was attached to the fuselage in either a mid or high position and an unswept horizontal tail was located on the fuselage center line. Two vertical tails were tested which had areas of 26.7 or 20.3 percent of the wing area. Each vertical tail was equipped with a rudder and had a geometric aspect ratio of 1.5, a taper ratio of 0.16, and 54 degrees of sweepback of the leading edge. Each vertical tail was tested at two different tail lengths. The wind-tunnel tests were conducted at a Reynolds number of 2.5 milMon at Mach numbers from 0.25 to 0.95.