Author: Dennis E. FullerPublisher:
ISBN:
Category : Mach number
Languages : en
Pages : 28
Book Description
Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63
Author: Dennis E. FullerPublisher:
ISBN:
Category : Mach number
Languages : en
Pages : 28
Book Description
Hypersonics Before the Shuttle: A Concise History of the X-15 Research Airplane
Author: Space Shuttle Missions Summary (NASA/TM-2011-216142)
Author: Robert D. LeglerPublisher: www.Militarybookshop.CompanyUK
ISBN: 9781782662235
Category : Science
Languages : en
Pages : 300
Book Description
Full color publication. This document has been produced and updated over a 21-year period. It is intended to be a handy reference document, basically one page per flight, and care has been exercised to make it as error-free as possible. This document is basically "as flown" data and has been compiled from many sources including flight logs, flight rules, flight anomaly logs, mod flight descent summary, post flight analysis of mps propellants, FDRD, FRD, SODB, and the MER shuttle flight data and inflight anomaly list. Orbit distance traveled is taken from the PAO mission statistics.
Atmospheric Re-Entry Vehicle Mechanics
Author: Patrick GallaisPublisher: Springer Science & Business Media
ISBN: 3540736476
Category : Technology & Engineering
Languages : en
Pages : 365
Book Description
Based on a long engineering experience, this book offers a comprehensive and state-of-the-art analysis of aerodynamic and flight mechanic entry topics. This updated edition had new chapters on Re-entry on Mars mission, flight quality, rarefied aerodynamics and re-entry accuracy. In addition, it provides a large set of application exercises and solutions.
On the Frontier
Author: Richard P. HallionPublisher:
ISBN:
Category : Flight
Languages : en
Pages : 420
Book Description
Computers Take Flight: A History of NASA's Pioneering Digital Fly-By-Wire Project
Author: James E. TomaykoPublisher:
ISBN:
Category : History
Languages : en
Pages : 210
Book Description
Hypersonic and High Temperature Gas Dynamics
Author: John David AndersonPublisher: AIAA
ISBN: 9781563474590
Category : Science
Languages : en
Pages : 710
Book Description
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.
Parachute Recovery Systems
Author: Theo W. KnackePublisher:
ISBN:
Category : Sports & Recreation
Languages : en
Pages : 524
Book Description
The purpose of this manual is to provide recovery system engineers in government and industry with tools to evaluate, analyze, select, and design parachute recovery systems. These systems range from simple, one-parachute assemblies to multiple-parachute systems, and may include equipment for impact attenuation, flotation, location, retrieval, and disposition. All system aspects are discussed, including the need for parachute recovery, the selection of the most suitable recovery system concept, concept analysis, parachute performance, force and stress analysis, material selection, parachute assembly and component design, and manufacturing. Experienced recovery system engineers will find this publication useful as a technical reference book; recent college graduates will find it useful as a textbook for learning about parachutes and parachute recovery systems; and technicians with extensive practical experience will find it useful as an engineering textbook that includes a chapter on parachute- related aerodynamics. In this manual, emphasis is placed on aiding government employees in evaluating and supervising the design and application of parachute systems. The parachute recovery system uses aerodynamic drag to decelerate people and equipment moving in air from a higher velocity to a lower velocity and to a safe landing. This lower velocity is known as rate of descent, landing velocity, or impact velocity, and is determined by the following requirements: (1) landing personnel uninjured and ready for action, (2) landing equipment and air vehicles undamaged and ready for use or refurbishment, and (3) impacting ordnance at a preselected angle and velocity.
A Review of High-speed, Convective, Heat-transfer Computation Methods
Author: Michael E. TauberPublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
Book Description
Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180°
Author: J. W. UsryPublisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 32
Book Description