| Referências |
| Por Bruno Ferreira Porto | |
| 04 de December de 2007 | |
|
Referências bibliográficas e eletrônicas deste site. Algumas possuem links para download na Internet.
1. Michaelis. Moderno Dicionário da Língua Portuguesa. São Paulo : Editora Melhoramentos Ltda., 2007.
6. Platzek, H. Preliminary Solid Rocket Motor Design Techiniques. China Lake, CA : Naval Weapons Center, 1979. 7. U.S. Army Missile Command. Design of Aerodynamically Stabilized Free Rockets. Redstone Arsenal : US Government Printng Office, 1990. 8. Sutton, George P. Rocket Propulsion Elements. Estados Unidos : John Wiley & Sons, Inc., 1963. 9. NASA. Solid propellant grain design and internal ballistics. s.l. : NASA, 1972. SP-8076.
10. Toft, Hans O. Voids in solid propellants. s.l. : DANSK AMATØR RAKET KLUB, 2002. 11. Moran, Michael J. e Shpairo, Howard N. Fundamentals of Engineering Thermodynamics. s.l. : John Wiley & Sons Ltd, 2006. ISBN-13 978-0-470-03037-0.
13. Gordon, Sanford e McBride, Bonnie J. Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications. s.l. : NASA, 1994. RP-1311. 14. NASA. Solid Rocket Motor Performance Analysis and Prediction. s.l. : Nasa, 1971. SP-8039.
15. Kuo, K. K. Fundamentals of Solid-propellant Combustion. New York : American Institute of Aeronautics and Astronautics Inc., 1995. PB96-131479. 16. Wang, N. F. e Feng, W. Theoretical and Experimental Research on the Throat to Port Area. Xi'an : Xi'an Modern Chemistry Research Institute, 1999. 17. NASA. Solid Propellente Selection and Chacterization. s.l. : NASA, 1971. SP-8064.
19. Rampichini, S., D., Ruspa e L.T., DeLuca. Acoustic Emission of Underwater Burning Solid Rocket Propellants. Milão : Laboratorio di Termofisica, Dipartimento di Energetica.
21. Sanches, Rafael A. K. Previsão do Empuxo de Motor-Foguete a Propelente Sólido. Curitiba : Universidade Federal do Paraná, 2005. 22. Saad, Michel A. Compressible Fluid Flow. New Jersey : Prentice-Hall, 1993. ISBN 0-13-161373-1. 23. Blake, A. Practical Stress Analysis in Engineering Design. New York : McGraw-Hill, 1990. 24. Young, W.C. e Budynas, R.G. Roark's Formulas for Stress and Strain. s.l. : McGraw-Hill, 2002.
26. U.S. Department of Defense. Metallic Materials and Elements for Aerospace Vehicle Structures. Washington : U.S. Department of Defense, 1994. MIL-HDBK-5G. 27. NASA. Solid Rocket Motor Igniters. s.l. : NASA, 1971. SP-8051.
28. Barrowman, James S. e Barrowman, Judith A. The Theoretical Prediction of the Center of Pressure. s.l. : NARAM-8 R&D, 1966. 29. Chinn, S. S. Missile Configuration Design. New York : McGraw-Hill, 1961. 30. Crowell, Sr. Gary A. The descriptive Geometry of Nose Cones. 1996. 31. NASA. Astronautic Structures Manual. Alabama : NASA, 1975. TMX-73305.
32. Gurkin, L. W. e Needleman, H. C. Aeroballistic Characteristics and Flight Test Results for Hawnk and Nike-Hawnk Sounding Rocket Vehices. s.l. : NASA. 33. Frank, Jørgen. Rocket motion during vertical powered and unpowered flight. s.l. : DARK, 2005.
36. NASA. Deployable Aerodynamic Deceleration Systems. s.l. : NASA, 1971. SP-8066.
38. Ashley, Clifford. Ashley Book of Knots. s.l. : Doubleday, 1944. ISBN-13: 978-0385040259. 39. Robart. 188VR AIR CONTROL KIT INSTALLATION INSTRUCTIONS. s.l. : Robart, 03.
42. Forest Products Laboratory. Wood handbook - Wood as an engineering material. Madison : s.n., 1999. 43. Shigley, Joseph E., Mischke, Charles R. e Budyans, Richard G. Projeto de Engenharia Mecânica. São Pulo : Bookman, 2005. ISBN 85-363-0562-2. 44. NASA. Solid Rocket Motors Metal Cases. s.l. : NASA, 1970. SP-8025.
45. Platzek, H. Preliminary Solid Rocket Motor Design Techniques. China Lake : Naval Weapons Center, 1975. NWC TM 2953.
47. Nakka, Richard A. Solid Propellant Rocket Motor Design and Testing. Manitoba : s.n., 1984. |
|
| Última Atualização ( 04 de December de 2007 ) |