Characteristics Of A Variable Geometry Entry Vehicle At Mach Numbers From 105 To 211 In Helium Flow
Download Characteristics Of A Variable Geometry Entry Vehicle At Mach Numbers From 105 To 211 In Helium Flow full books in PDF, epub, and Kindle. Read online free Characteristics Of A Variable Geometry Entry Vehicle At Mach Numbers From 105 To 211 In Helium Flow ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads.
Author |
: |
Publisher |
: |
Total Pages |
: 46 |
Release |
: 1964 |
ISBN-10 |
: NASA:31769000663735 |
ISBN-13 |
: |
Rating |
: 4/5 (35 Downloads) |
Synopsis Characteristics of a Variable-geometry Entry Vehicle at Mach Numbers from 10.5 to 21.1 in Helium Flow by :
Author |
: Patrick J. Johnston |
Publisher |
: |
Total Pages |
: 26 |
Release |
: 1960 |
ISBN-10 |
: NASA:31769000454630 |
ISBN-13 |
: |
Rating |
: 4/5 (30 Downloads) |
Synopsis Effect of a Variable-geometry Diffuser on the Operating Characteristics of a Helium Tunnel Designed for a Mach Number in Excess of 20 by : Patrick J. Johnston
Author |
: |
Publisher |
: |
Total Pages |
: 36 |
Release |
: 1965 |
ISBN-10 |
: NASA:31769000665151 |
ISBN-13 |
: |
Rating |
: 4/5 (51 Downloads) |
Synopsis Stability Characteristics of a Manned Lifting Entry Vehicle at a Mach Number of 20.3 Helium by :
Author |
: Roger H. Fournier |
Publisher |
: |
Total Pages |
: 76 |
Release |
: 1967 |
ISBN-10 |
: NASA:31769000666878 |
ISBN-13 |
: |
Rating |
: 4/5 (78 Downloads) |
Synopsis Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Variable-geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control by : Roger H. Fournier
An investigation of a lifting body configuration has been conducted in the Langley Unitary Plan wind tunnel through a Mach number range from 1.50 to 4.63 to determine the control effectiveness characteristics of body base flaps with and without anhedral tail elevator controls.
Author |
: Melvin J. Fohrman |
Publisher |
: |
Total Pages |
: 48 |
Release |
: 1963 |
ISBN-10 |
: UIUC:30112106874081 |
ISBN-13 |
: |
Rating |
: 4/5 (81 Downloads) |
Synopsis Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium by : Melvin J. Fohrman
Author |
: |
Publisher |
: |
Total Pages |
: 68 |
Release |
: 1963 |
ISBN-10 |
: NASA:31769000662174 |
ISBN-13 |
: |
Rating |
: 4/5 (74 Downloads) |
Synopsis Summary of Aerodynamic Characteristics of a Winged Reentry Vehicle at Mach Numbers from 0.06 to 9.6 with Detailed Results at a Mach Number of 9.6 by :
Author |
: Harvey H. Hubbard |
Publisher |
: |
Total Pages |
: 620 |
Release |
: 1991 |
ISBN-10 |
: STANFORD:36105024722329 |
ISBN-13 |
: |
Rating |
: 4/5 (29 Downloads) |
Synopsis Aeroacoustics of Flight Vehicles by : Harvey H. Hubbard
Author |
: John David Anderson |
Publisher |
: AIAA |
Total Pages |
: 710 |
Release |
: 1989 |
ISBN-10 |
: 156347459X |
ISBN-13 |
: 9781563474590 |
Rating |
: 4/5 (9X Downloads) |
Synopsis Hypersonic and High Temperature Gas Dynamics by : John David Anderson
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.
Author |
: Nasa |
Publisher |
: PDQ Press |
Total Pages |
: 400 |
Release |
: 2009 |
ISBN-10 |
: 0979828899 |
ISBN-13 |
: 9780979828898 |
Rating |
: 4/5 (99 Downloads) |
Synopsis Columbia Crew Survival Investigation Report by : Nasa
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.
Author |
: Dan M. Goebel |
Publisher |
: John Wiley & Sons |
Total Pages |
: 528 |
Release |
: 2008-12-22 |
ISBN-10 |
: 9780470436264 |
ISBN-13 |
: 0470436263 |
Rating |
: 4/5 (64 Downloads) |
Synopsis Fundamentals of Electric Propulsion by : Dan M. Goebel
Throughout most of the twentieth century, electric propulsion was considered the technology of the future. Now, the future has arrived. This important new book explains the fundamentals of electric propulsion for spacecraft and describes in detail the physics and characteristics of the two major electric thrusters in use today, ion and Hall thrusters. The authors provide an introduction to plasma physics in order to allow readers to understand the models and derivations used in determining electric thruster performance. They then go on to present detailed explanations of: Thruster principles Ion thruster plasma generators and accelerator grids Hollow cathodes Hall thrusters Ion and Hall thruster plumes Flight ion and Hall thrusters Based largely on research and development performed at the Jet Propulsion Laboratory (JPL) and complemented with scores of tables, figures, homework problems, and references, Fundamentals of Electric Propulsion: Ion and Hall Thrusters is an indispensable textbook for advanced undergraduate and graduate students who are preparing to enter the aerospace industry. It also serves as an equally valuable resource for professional engineers already at work in the field.