REFERENCES
- Anderson , J. B. and Reichenbach , R. E. ( 1966 ). 76-inch Diameter Centrifuge Facility , Naval Postgraduate School Technical Note No. TN 66T-4 .
- Anderson , J. B. and Reichenbach , R. E. ( 1968 ). An Investigation of the Effect of Acceleration on the Burning Rate of Composite Propellants . AIAA Journal 6 , 271 .
- ASTM Publication PD1S-181 , 1968 , Inorganic Index to the Powder Diffraction File 1968 ,
- Boggs , T. L. , Derr , R. L. and Beckstead , M. W. ( 1970 ). Surface Structure of Ammonium Perchloratc Composite Propellants . AIAA Journal 8 , 370 .
- Broddner , S. ( 1970 ). Effects of High Spin on the Internal Ballistics of a Solid Rocket Motor , Astronautica Acta 15 , 191 .
- Crowe , C. T. and Willoughby , P. G. ( 1966 ). Effect of Spin on the Internal Ballistics of a Solid Rocket Motor , AIAA Paper No. 66–523 .
- Fenn , J. B. ( 1967 ). A Phalanx Flame Model for the Combustion of Composite Solid Propellants , Project Squid Technical Resport PR-1 14-P .
- Glick , R. L. ( 1966 ). An Analytical Study of the Effects of Radial Acceleration Upon the Combustion Mechanism of Solid Propellant , Contract NAS7–406, NASA Report No. 66218, Thiokol Report No. 42–.6 .
- Glick , R. L. ( 1971 ). Comment on An Investigation of the Acceleration Induced Burning Rate Increase of Nonmetalized Composite Propellants . AIAA Journal 9 , 542 .
- Hightower , J. D. and Price , E. W. ( 1968 ). Experimental Studies Relating to the Combustion Mechanism of Composite Propellants , Astronautica Acta 14 , 11 .
- King , M. K. and McHale , E. T. ( 1969 ). An Optical Bomb Study of the Combustion of Solid Propellants in High Acceleration Fields , Atlantic Research Corporation , Second Annual Technical Report .
- Nagaoka , T. , Ito , K. and Koreki , T. ( 1969 ). Combustion of Propellant Under Spin Acceleration , 8th International Symposium on Space Technology and Science , Tokyo , Japan , AGNE Publications, Inc .
- Northam , G. B. ( 1968 ). Effects of Steady-State Acceleration on Combustion Characteristics of an Bluminized Composite Solid Propellant . NASA TN D-4914 .
- Northam , G. B. ( 1969 ). Acceleration-Induced Transient Burning-Rate Augmentation of An Aluminized Solid Rocket Propellant , Ph.D. Thesis , Virginia Polytechnic Institute .
- Northam , G. B. and Lucy , M. H. ( 1968 ). On the Effects or Acceleration Upon Solid Rocket Performance , AIAA Paper No. 68–530 .
- Northam , G.B. and Lucy , M. H. ( 1969 ). Effects of Acceleration Upon Solid Rocket Performance . Journal of Spacecraft and Rockets 6 , 456 .
- Sturm , E. J. and Reichenbach , R. E. ( 1968 ). An Experimental Study of the Burning Rates of Aluminized Composite Solid Propellants in Acceleration Fields , AIAA Paper No. 68–529 .
- Sturm , E. J. and Reichenbach , R. E. ( 1970 ). An Investigation of the Acceleration Induced Burning Rate Increase of Non-metallized Composite Propellants . AIAA Journal 8 , 1062 .
- Summerfield , M. , et al. ( 1960 ). Burning Mechanism of Ammonium Perchlorate Propellants , Progress in Astronautics and Rocketry , Vol. 1 , New York Academic Press , p. 142 .
- Willoughby , P. G. , Baker , K. L. and Hermsen , R. W. ( 1969 ). Photographic Study of Solid Propellants Burning In An Acceleration Environment , UTC Contractor Report for NASA , NASA CR-66824 .
- Willoughby , P. G. , Crowe , C. T. and Baker , K. L. ( 1969 ). A Photographic and Analytical Study of Composite Propellant Combustion In An Acceleration Field , Journal of Spacecraft and Rockets 8 , 310 .