000			03693nam a22004573i 4500
001			EBC3111458
003			MiAaPQ
005			20240729124518.0
006			m o d |
007			cr cnu||||||||
008			240724s1996 xx o ||||0 eng d
020			_a9781600861161 _q(electronic bk.)
020			_z9781563471285
035			_a(MiAaPQ)EBC3111458
035			_a(Au-PeEL)EBL3111458
035			_a(CaPaEBR)ebr10516440
035			_a(OCoLC)922978753
040			_aMiAaPQ _beng _erda _epn _cMiAaPQ _dMiAaPQ
050		4	_aTL782 -- .B68 1996eb
082	0		_a629.47/5
100	1		_aBrown, Charles D.
245	1	0	_aSpacecraft Propulsion.
250			_a1st ed.
264		1	_aReston : _bAmerican Institute of Aeronautics and Astronautics, _c1996.
264		4	_c©1996.
300			_a1 online resource (237 pages)
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
490	1		_aAIAA Education Series
505	0		_aCover -- Half Title -- Title Page -- Copyright Page -- Series Page -- Table of Contents -- Foreword -- Preface -- About the Author -- Chapter 1: Introduction -- 1.1 History of Rocket Propulsion -- 1.2 Propulsion System Types -- 1.3 PRO: AIAA Propulsion Design Software -- 1.4 Arrangement of the Book -- Chapter 2: Theoretical Rocket Performance -- 2.1 Thrust -- 2.2 Ideal Rocket Thermodynamics -- Problems -- Chapter 3: Propulsion Requirements -- 3.1 Mission Design -- 3.2 Changes in Orbit -- 3.3 Plane Changes -- 3.4 Orbit Trim -- 3.5 Repositioning -- 3.6 Attitude Maneuvers -- 3.7 Limit Cycles -- 3.8 Reaction Wheel Unloading -- Problems -- Chapter 4: Monopropellant Systems -- 4.1 Monopropellant Hydrazine Thrusters -- 4.2 Electrothermal and Arcjet Thrusters -- 4.3 Propellant Systems -- 4.4 Pressurization Subsystems -- 4.5 Tankage -- 4.6 Monopropellant System Design Example -- 4.7 Flight Mono propellant Systems -- Problems -- Chapter 5: Bipropellant Systems -- 5.1 Bipropellant Rocket Engines -- 5.2 Bipropellants -- 5.3 Bipropellant Fluid Systems -- 5.4 Launch Vehicle Systems -- 5.5 Dual-Mode Systems -- 5.6 Flight Bipropellant Systems -- Problems -- Chapter 6: Solid Rocket Systems -- 6.1 Propellants -- 6.2 Grains -- 6.3 Thrust Control -- 6.4 Cases -- 6.5 Nozzles -- 6.6 Performance -- 6.7 Some Flight Motors -- Problems -- Chapter 7: Cold-Gas Systems -- 7.1 Design Considerations -- 7.2 Flight Systems -- Appendix A: PRO: AIAA Propulsion Design Software -- A.1 Introduction to PRO -- A.2 Quick Tour of PRO: AIAA Propulsion Design Software -- A.3 The Main Menu -- A.4 Propulsion Requirements -- A.5 Rocket Engine Design -- A.6 Pulsing Engine Performance -- A.7 Blowdown System Performance -- A.8 System Weight Statement -- A.9 Utilities -- A.10 Sample Problems -- A.11 Hard Drive Installation -- Appendix B: Propulsion Design Data -- B.1 Conversion Factors.
505	8		_aB.2 Propellant Properties -- 8.3 PRO: Files -- 8.4 Planetary Data -- Appendix C: Glossary -- References -- Index.
588			_aDescription based on publisher supplied metadata and other sources.
590			_aElectronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
650		0	_aSpace vehicles -- Propulsion systems.
655		4	_aElectronic books.
776	0	8	_iPrint version: _aBrown, Charles D. _tSpacecraft Propulsion _dReston : American Institute of Aeronautics and Astronautics,c1996 _z9781563471285
797	2		_aProQuest (Firm)
830		0	_aAIAA Education Series
856	4	0	_uhttps://ebookcentral.proquest.com/lib/orpp/detail.action?docID=3111458 _zClick to View
999			_c68126 _d68126