Author: Publisher:
ISBN:
Category : Space shuttles
Languages : en
Pages : 540
Book Description
Space Shuttle Technical Conference, Part 2
Author: Space Shuttle Technical Conference, Part 1
Author: NASA Space Shuttle Technology Conference. Volume 2 - Structures and Materials
Author: Publisher:
ISBN:
Category : Reusable space vehicles
Languages : en
Pages : 652
Book Description
Space Shuttle Technical Conference
Author: NASA Scientific and Technical Publications
Author: Scientific and Technical Aerospace Reports
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.
Langley's Space Shuttle Technology: A Bibliography
Author: Gloria R. ChampinePublisher:
ISBN:
Category : Space shuttles
Languages : en
Pages : 74
Book Description
Aerospace Engineering on the Back of an Envelope
Author: Irwin E. AlberPublisher: Springer Science & Business Media
ISBN: 3642225373
Category : Technology & Engineering
Languages : en
Pages : 326
Book Description
Engineers need to acquire “Back-of-the-Envelope” survival skills to obtain rough quantitative answers to real-world problems, particularly when working on projects with enormous complexity and very limited resources. In the case studies treated in this book, we show step-by-step examples of the physical arguments and the resulting calculations obtained using the quick-fire method. We also demonstrate the estimation improvements that can be obtained through the use of more detailed physics-based Back-of-the-Envelope engineering models. These different methods are used to obtain the solutions to a number of design and performance estimation problems arising from two of the most complex real-world engineering projects: the Space Shuttle and the Hubble Space Telescope satellite.
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