Future Spacecraft Propulsion Systems and Integration (Record no. 80794)

000 -LEADER
fixed length control field 03601nam a22005775i 4500
001 - CONTROL NUMBER
control field 978-3-662-54744-1
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20220801222448.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 170831s2018 gw | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783662547441
-- 978-3-662-54744-1
082 04 - CLASSIFICATION NUMBER
Call Number 629.1
100 1# - AUTHOR NAME
Author Czysz, Paul A.
245 10 - TITLE STATEMENT
Title Future Spacecraft Propulsion Systems and Integration
Sub Title Enabling Technologies for Space Exploration /
250 ## - EDITION STATEMENT
Edition statement 3rd ed. 2018.
300 ## - PHYSICAL DESCRIPTION
Number of Pages LXI, 463 p. 349 illus.
490 1# - SERIES STATEMENT
Series statement Astronautical Engineering,
505 0# - FORMATTED CONTENTS NOTE
Remark 2 Overview -- Our progress appears to be impeded -- Commercial near-Earth space launcher: a perspective -- Commercial near-Earth launcher: propulsion -- Earth orbit on-orbit operations in near-Earth orbit, a necessary second step -- Earth-Moon system: establishing a Solar System presence -- Exploration of our Solar System -- Stellar and interstellar precursor missions -- View to the future and exploration of our Galaxy.
520 ## - SUMMARY, ETC.
Summary, etc The updated and expanded third edition of this book focuses on the multi-disciplinary coupling between flight-vehicle hardware alternatives and enabling propulsion systems. It discusses how to match near-term and far-term aerospace vehicles to missions and provides a comprehensive overview of the subject, directly contributing to the next-generation space infrastructure, from space tourism to space exploration. This holistic treatment defines a mission portfolio addressing near-term to long-term space transportation needs covering sub-orbital, orbital and escape flight profiles. In this context, a vehicle configuration classification is introduced covering alternatives starting from the dawn of space access. A best-practice parametric sizing approach is introduced to correctly design the flight vehicle for the mission. This technique balances required mission with the available vehicle solution space and is an essential capability sought after by technology forecasters and strategic planners alike.
700 1# - AUTHOR 2
Author 2 Bruno, Claudio.
700 1# - AUTHOR 2
Author 2 Chudoba, Bernd.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier https://doi.org/10.1007/978-3-662-54744-1
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Berlin, Heidelberg :
-- Springer Berlin Heidelberg :
-- Imprint: Springer,
-- 2018.
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-- text
-- txt
-- rdacontent
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-- computer
-- c
-- rdamedia
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-- online resource
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347 ## -
-- text file
-- PDF
-- rda
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Astronautics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Solar system.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace Technology and Astronautics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Space Physics.
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
-- 2365-9602
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-- ZDB-2-ENG
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-- ZDB-2-SXE

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