|
|
|
|
LEADER |
04923nam a2200685 4500 |
001 |
ocn869881452 |
003 |
OCoLC |
005 |
20170124072523.3 |
006 |
m o d |
007 |
cr ||||||||||| |
008 |
140203s2014 nju o 001 0 eng |
010 |
|
|
|a 2014004797
|
040 |
|
|
|a DLC
|b eng
|e rda
|c DLC
|d YDX
|d EBLCP
|d N$T
|d IDEBK
|d YDXCP
|d CUI
|d CDX
|d RECBK
|d E7B
|d COO
|d DEBSZ
|d DEBBG
|d DG1
|d GrThAP
|
019 |
|
|
|a 884595177
|
020 |
|
|
|a 9781118855317 (ePub)
|
020 |
|
|
|a 1118855310 (ePub)
|
020 |
|
|
|a 9781118854976 (Adobe PDF)
|
020 |
|
|
|a 1118854977 (Adobe PDF)
|
020 |
|
|
|z 9781118853870 (cloth)
|
020 |
|
|
|a 1118853873
|
020 |
|
|
|a 9781118855065
|
029 |
1 |
|
|a NZ1
|b 15753478
|
029 |
1 |
|
|a NZ1
|b 15906996
|
029 |
1 |
|
|a CHVBK
|b 334093813
|
029 |
1 |
|
|a CHBIS
|b 010442115
|
029 |
1 |
|
|a DEBSZ
|b 431707847
|
029 |
1 |
|
|a DEBBG
|b BV042989824
|
035 |
|
|
|a (OCoLC)869881452
|z (OCoLC)884595177
|
042 |
|
|
|a pcc
|
043 |
|
|
|a zmo----
|
050 |
0 |
0 |
|a TL1075
|
072 |
|
7 |
|a TEC
|x 009000
|2 bisacsh
|
082 |
0 |
0 |
|a 629.4/11
|2 23
|
049 |
|
|
|a MAIN
|
100 |
1 |
|
|a Parker, Jeffrey S.
|
245 |
1 |
0 |
|a Low-energy lunar trajectory design /
|c Jeffrey S. Parker and Rodney L. Anderson.
|
264 |
|
1 |
|a Hoboken, New Jersey :
|b Wiley,
|c [2014]
|
300 |
|
|
|a 1 online resource.
|
336 |
|
|
|a text
|2 rdacontent
|
337 |
|
|
|a computer
|2 rdamedia
|
338 |
|
|
|a online resource
|2 rdacarrier
|
490 |
1 |
|
|a Deep-space communications and navigation series
|
500 |
|
|
|a Includes index.
|
588 |
|
|
|a Description based on print version record and CIP data provided by publisher.
|
504 |
|
|
|a Includes bibliographical references and index.
|
520 |
|
|
|a "Based on years of research conducted at the NASA Jet Propulsion Laboratory, Low-Energy Lunar Trajectory Design provides high-level information to mission managers and detailed information to mission designers about low-energy transfers between Earth and the moon. The book answers high-level questions about the availability and performance of such transfers in any given month and year. Low-energy lunar transfers are compared with various other types of transfers, and placed within the context of historical missions. Using this book, designers may reconstruct any transfer described therein, as well as design similar transfers with particular design parameters." --
|c Portion of summary from book.
|
505 |
0 |
|
|a Half Title page; Title page; Copyright page; Dedication; Foreword; Preface; Acknowledgments; Authors; Chapter 1: Introduction And Executive Summary; 1.1 Purpose; 1.2 Organization; 1.3 Executive Summary; 1.4 Background; 1.5 The Lunar Transfer Problem; 1.6 Historical Missions; 1.7 Low-Energy Lunar Transfers; Chapter 2: Methodology; 2.1 Methodology Introduction; 2.2 Physical Data; 2.3 Time Systems; 2.4 Coordinate Frames; 2.5 Models; 2.6 Low-Energy Mission Design; 2.7 Tools; Chapter 3: Transfers To Lunar Libration Orbits; 3.1 Executive Summary; 3.2 Introduction
|
505 |
8 |
|
|a 3.3 Direct Transfers Between Earth And Lunar Libration Orbits3.4 Low-Energy Transfers Between Earth And Lunar Libration Orbits; 3.5 Three-Body Orbit Transfers; Chapter 4: Transfers To Low Lunar Orbits; 4.1 Executive Summary; 4.2 Introduction; 4.3 Direct Transfers Between Earth And Low Lunar Orbit; 4.4 Low-Energy Transfers Between Earth And Low Lunar Orbit; 4.5 Transfers Between Lunar Libration Orbits And Low Lunar Orbits; 4.6 Transfers Between Low Lunar Orbits And The Lunar Surface; Chapter 5: Transfers To The Lunar Surface; 5.1 Executive Summary
|
505 |
8 |
|
|a 5.2 Introduction For Transfers To The Lunar Surface5.3 Methodology; 5.4 Analysis Of Planar Transfers Between The Earth And The Lunar Surface; 5.5 Low-Energy Spatial Transfers Between The Earth And The Lunar Surface; 5.6 Transfers Between Lunar Libration Orbits And The Lunar Surface; 5.7 Transfers Between Low Lunar Orbits And The Lunar Surface; 5.8 Conclusions Regarding Transfers To The Lunar Surface; Chapter 6: Operations; 6.1 Operations Executive Summary; 6.2 Operations Introduction; 6.3 Launch Sites; 6.4 Launch Vehicles; 6.5 Designing A Launch Period; 6.6 Navigation
|
505 |
8 |
|
|a 6.7 Spacecraft Systems DesignAppendix A: Locating the Lagrange Points; A.1 Introduction; A.2 Setting Up The System; A.3 Triangular Points; A.4 Collinear Points; A.5 Algorithms; References; Terms; Constants; Index
|
650 |
|
0 |
|a Lunar probes
|x Trajectories.
|
650 |
|
0 |
|a Space flight to the moon
|x Cost control.
|
650 |
|
7 |
|a TECHNOLOGY & ENGINEERING
|x Engineering (General)
|2 bisacsh
|
655 |
|
4 |
|a Electronic books.
|
655 |
|
0 |
|a Electronic books.
|
700 |
1 |
|
|a Anderson, Rodney L.
|
776 |
0 |
8 |
|i Print version:
|a Parker, Jeffrey S.
|t Low-energy lunar trajectory design
|d Hoboken, New Jersey : John Wiley & Sons Inc., [2014]
|z 9781118853870
|w (DLC) 2014001158
|
830 |
|
0 |
|a Deep-space communications and navigation series.
|
856 |
4 |
0 |
|u https://doi.org/10.1002/9781118855065
|z Full Text via HEAL-Link
|
994 |
|
|
|a 92
|b DG1
|