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MIL-HDBK-762 Base Document:1990

Current

Current

The latest, up-to-date edition.

Design of Aerodynamically Stabilized Free Rockets

Available format(s)

PDF

Published date

17-07-1990

€17.95
Excluding VAT

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.

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

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.

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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