Design of Aerodynamically Stabilized Free Rockets

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Published date

17-07-1990

Publisher

US Military Specs/Standards/Handbooks

FOREWORD
LIST OF ILLUSTRATIONS
LIST OF TABLES
LIST OF ABBREVIATIONS AND ACRONYMS
CHAPTER 1 - INTRODUCTION
CHAPTER 2 - SYSTEM DESIGN
CHAPTER 3 - PERFORMANCE
CHAPTER 4 - ACCURACY
CHAPTER 5 - AERODYNAMICS
CHAPTER 6 - PROPULSION
CHAPTER 7 - STRUCTURES
CHAPTER 8 - LAUNCHER CONSIDERATIONS
APPENDIX A - ATMOSPHERIC DATA
APPENDIX B - COMPUTER PROGRAMS
APPENDIX C - HEAT TRANSFER EQUATIONS
REFERENCES
BIBLIOGRAPHY
INDEX

Describes the conceptual and preliminary design phases; however, reference is made to the technical approaches and computer programs required for the system development phase.

Aerodynamically stabilized free rockets offer relatively simple, reliable, small, low-cost means for delivering payloads and, when great accuracy is not required, are often the optimum systems. This handbook provides engineering design information and data for such rockets. Primarily, this handbook is intended to cover the conceptual and preliminary design phases; however, reference is made to technical approaches and computer programs required for the system development phase. The material includes operational and interface requirements as they influence the design of the total weapon system.

DevelopmentNote	NOTICE 1 - Notice of Validation. (05/2001) NOTICE 2 - Notice of Validation. (03/2006) NOTICE 3 - Notice of Validation. (10/2013)
DocumentType	Standard
Pages	721
PublisherName	US Military Specs/Standards/Handbooks
Status	Current

MIL HDBK 5 : G_VOL2	METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES
MIL-STD-286 Revision C:1991	PROPELLANTS, SOLID: SAMPLING, EXAMINATION AND TESTING
MIL-HDBK-727 Base Document:1984	DESIGN GUIDANCE FOR PRODUCIBILITY
MIL-STD-961 Revision E:2003	DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT

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MIL-HDBK-762 Base Document:1990

Design of Aerodynamically Stabilized Free Rockets

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