list of publications - shodhgangashodhganga.inflibnet.ac.in/bitstream/10603/8545/18/18... ·...

187

LIST OF PUBLICATIONS

1. Ram Mohan.CH.V, Ramanathan.J, Sathish Kumar, Gupta

.A.V.S.S.K.S, “Characterization of Materials used in Flex Bearings

of Large Solid Rocket Motors”,Defence Science Journal, Vol 61, No

03, May 2011, PP264-269.

2. Nagendranath.A., Rao.N.V.M., Ram Mohan.CH.V.,

Gupta.R.K.,”Large Diameter Rocket Motor Casing Joint Analysis”,

Aero Tech, 2008, National Seminar on ‘Recent Advances in

Aerospace Technologies, Maintenance and Optimization’,

November 14-15, 2008

3. Ram Mohan.CH.V., Govind Rao,Brahmanandam.P.V.G,

Sekaran.V.G, ”Testing of Flex Seals of Large Solid Rocket Motors”,

Journal of Aerospace Quality and Reliability, Vol. 2. No. 1,

January 2006, pp. 61-71.

LIST OF REFERENCES

1. Nagappa,R., Kunup,M.R., Muthunayagam,A,E., “ISRO’s Solid

Rocket Motors”, Acta Astronautica, Volume 19, Issue 8, August

1989, Pages 681-697.

2. Leonard H. Caveny, Robert L. Geisler, Russell A. Ellis, Thomas L.

Moore, "Solid Rocket Enabling Technologies and Milestones in the

United States", Journal of Propulsion and Power 2003, vol.19

no.6 pp-1038-1066

188

3. Kennedy, W. S., Kovacic, S. M., Rea, E. C., ”Solid rocket history at

TRW Ballistic Missiles Division”, AIAA-1992-3614, SAE, ASME,

and ASEE, Joint Propulsion Conference and Exhibit, 28th,

Nashville, TN, July 6-8, 1992.

4. Dautriat, Eric, Tuchot, Andre, “Solid propulsion systems for small

launchers derived from Ariane 5”, AIAA-1992-3306, SAE, ASME,

and ASEE, Joint Propulsion Conference and Exhibit, 28th,

Nashville, TN, July 6-8, 1992.

5. Alain Mercier, aurelie Esnault, Didier Boury, Philippe clouted,

Laurence Guenot, Christophe Talbot, “Application of recent

technologies for the next generation solid rocket motors”, 57th

International Astronautical Congress, Valencia, Spain, Oct. 2-6,

2006.

6. Fukushima, Yukio, Fujita, Takeshi, Nagatomo, Masanori, "H-II

solid rocket booster design and development ",AIAA-1995-2738 ,

ASME, SAE, and ASEE, Joint Propulsion Conference and Exhibit,

31st, San Diego, CA, July 10-12, 1995

7. Carroll, H. B, Godfrey, J. S, Crum, J. F "Design and development

of Pegasus propulsion", AIAA-1989-2314, ASME, SAE, and ASEE,

Joint Propulsion Conference, 25th, Monterey, CA, July 10-13,

1989.

8. Fleischman, T. T, Vincent, E. O, "MX stage II propulsion, total

system concept ", AIAA-1980-1183, SAE, and ASME, Joint

189

Propulsion Conference, 16th, Hartford, Conn., June 30-July 2,

1980.

9. Thomas Rudman, “Titan IV - History and Final Flights”, AIAA-

2002-4205, 38th AIAA/ASME/SAE/ASEE Joint Propulsion

Conference and Exhibit, Indianapolis, Indiana, July 7-10, 2002.

10. Jason Andrews, Livingston Holder, “Propulsion System Design for

the Peregrine Launch System”, AIAA-2004-3906, 40th

AIAA/ASME/SAE/ASEE Joint Propulsion Conference and

Exhibit, Fort Lauderdale, Florida, July 11-14, 2004.

11. S.S. Balakrishnan, "PSVL - a Low Cost Launcher & Evolution of

Indian Launchers" 54th International Astronautical Congress of

the International Astronautical Federation, the International

Academy of Astronautics, and the International Institute of Space

Law, Bremen, Germany, Sep. 29-30, 2003.

12. Coleman, M., ”U.S. expendable launch vehicle performance

history”, AIAA-2000-3281, AIAA, ASME, SAE, ASEE Joint

Propulsion Conference and Exhibit, 36th, Huntsville, AL, July 16-

19, 2000

13. Perroten.G, Boury.D, Astorg.J.M, Beyeldieu.E, “The European

Small Launcher - A design to cost launch”, AIAA-1995-3770

,AIAA Space Programs and Technologies Conference, Huntsville,

AL, Sept 26-28, 1995

14. Stoecker, Ted, Frazier, Scott , Padavano, Joe, "The Taurus

Launch Vehicle design and capability", AIAA-1992-3868, SAE,

190

ASME, and ASEE, Joint Propulsion Conference and Exhibit, 28th,

Nashville, TN, July 6-8, 1992. 15 p.

15. R. A. Fuhrman, "The Fleet Ballistic Missile System - Polaris to

Trident", AIAA-1978-355, Journal of Spacecraft and Rockets, Feb

7-9, 1978.

16. A.I.El-Sharkawy,“Experimental studies on thrust vector control in

solid propellant rockets”, AIAA-1977-989, American Institute of

Aeronautics and Astronautics and Society of Automotive

Engineers, Propulsion Conference, 13th, Orlando, Fla., July 11-

13, 1977.

17. Caton, J. L., Franke, M. E., ”Two-dimensional thrust vector

control nozzle”, AIAA-1991-2101,SAE, ASME, and ASEE, Joint

Propulsion Conference, 27th, Sacramento, CA, June 24-26, 1991.

18. Cavalleri, Robert, Tiarn, Weihnurng, “Experimental and

theoretical comparison of the Probe Thrust Vector Control

concept”, AIAA-1991-2476, SAE, ASME, and ASEE, Joint

Propulsion Conference, 27th, Sacramento, CA, June 24-26, 1991.

19. Ryan, R. W., Franke, M. “Dynamic response of an axisymmetric

thrust vector control nozzle”, AIAA-1991-344, Aerospace Sciences

Meeting, 29th, Reno, NV, Jan 7-10, 1991.

20. Schoeyer, “Thrust Vector Control for (clustered modules) plug

nozzles - Some considerations”, AIAA-1997-2823,


Exhibit, 33rd, Seattle, WA, July 6-9, 1997.

191

21. Wassom, Steven R, Perley.TIM, "Integrated aerofin/thrust vector

control for tactical missiles", Journal of Propulsion and Power

1991, Vol.7, No.3, pp-374-381

22. Wie, B, "Thrust vector control design for a liquid upper stage

spacecraft", AIAA-1985-1914, Guidance, Navigation and Control

Conference, Snowmass, CO, Aug 19-21, 1985. Journal of

Guidance, Control, and Dynamics.

23. Talda, T. A, Franke, M. E, " Two-dimensional confined jet thrust

vector control", AIAA-1989-2813, ASME, SAE, and ASEE, Joint

Propulsion Conference, 25th, Monterey, CA, July 10-13, 1989.

24. R. Akiba, M. Kohno, H. Inohara, T. Fujiwara, T. Murakami,

“Development of movable nozzle for Solid Rocket Motor”. AIAA,

1983-2285, Guidance and control conference, New York, August

15-17, 1983.

25. Alain de Champlain, Vincent Harrisson, ”Optical Technique to

Quantify Erosion on Jet Vanes for Thrust Vector Control”, AIAA-

2002-4190 ,38th AIAA/ASME/SAE/ASEE Joint Propulsion

Conference and Exhibit, Indianapolis, Indiana, July 7-10, 2002

26. Hong-Gye, Yong-Seok , "Thrust Vector Control Characteristics of

Jet Vanes Arranged with X-Formation Within a TVC Shroud",

AIAA-2003-5243, 39th AIAA/ASME/SAE/ASEE Joint Propulsion

Conference and Exhibit, Huntsville, Alabama, July 20-23, 2003

27. Vincent Harrisson , Alain de Champlain "Force Measurements

Evaluating Erosion Effects on Jet Vanes Thrust Vector Control

192

System ", AIAA-2003-5237, 39th AIAA/ASME/SAE/ASEE Joint

Propulsion Conference and Exhibit, Huntsville, Alabama, July 20-

23, 2003

28. Hong-Gye Sung , Yong-Seok , "Thrust-Vector Characteristics of

Jet Vanes Arranged in X-Formation Within a Shroud" Journal of

Propulsion and Power 2004, Vol.20, No.3, pp-501-508

29. Rahaim, Christopher P, Cavalleri, Robert J, " Jet vane thrust

vector control - A design effort" , AIAA-1996-2904, ASME, SAE,

and ASEE, Joint Propulsion Conference and Exhibit, 32nd, Lake

Buena Vista, FL, July 1-3, 1996

30. Divo, Eduardo, Cavalleri, Robert, "BEM model of ablation

characteristics of a thrust vector control vane"

AIAA-1998-2578 ,AIAA/ASME Joint Thermophysics and Heat

Transfer Conference, 7th, Albuquerque, NM, June 15-18, 1998

31. Zeamer, R. J, "Thrust vector control by liquid injection for solid

propellant rockets", AIAA-1975-1225, American Institute of


Engineers, Propulsion Conference, 11th, Anaheim, Calif., Sept

29-Oct 1, 1975.

32. Mark Mason, William Crowther , "Fluidic Thrust Vectoring for

Low Observable Air Vehicles", AIAA-2004-2210, 2nd AIAA Flow

Control Conference, Portland, Oregon, June 28-1, 2004.

33. Chiarelli, Charles, Johnsen, Raymond K, "Fluidic scale model

multi-plane thrust vector control test results", AIAA-1993-2433,

193

29th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and

Exhibit, Moneterey, CA, June 28-30, 1993

34. Erinc Erdem, Kahraman Albayrak , "Parametric Study of

Secondary Gas Injection into a Conical Rocket Nozzle for Thrust

Vectoring", AIAA-2006-4942 ,42nd AIAA/ASME/SAE/ASEE Joint

Propulsion Conference and Exhibit, Sacramento, California, July

9-12, 2006

35. E. Glenn Case, "Preliminary Design of a Hybrid Rocket Liquid

Injection Thrust Vector Control System", AIAA-2008-1420 , 46th

AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada,

Jan. 7-10, 2008

36. Huang, W.-H., "Nozzle erosion induced by thrust vector control

injection", AIAA-1996-2638, ASME, SAE, and ASEE, Joint

Propulsion Conference and Exhibit, 32nd, Lake Buena Vista, FL,

July 1-3, 1996

37. Hyun Ko, Woong-Sup Yoon, "Performance Analysis of Secondary

Gas Injection into a Conical Rocket Nozzle” Journal of Propulsion

and Power 2002 ,Vol.18, No.3, pp-585-591

38. Berdoyes, Michel , “Hot gas thrust vector control motor “, AIAA-

1992-3551, SAE, ASME, and ASEE, Joint Propulsion Conference

and Exhibit, 28th, Nashville, TN, July 6-8, 1992.

39. Balu, R, Marathe, A. G, Paul, P. J, Mukunda. H. S, "Analysis of

performance of a hot gas injection thrust vector Control system ",

Journal of Propulsion and Power 1991, Vol.7 , No.4, pp-580-585.

194

40. Woodberry, “Solid Rocket Thrust Vector Control”, NASA SP-8114,

December, 1974

41. Russel. A. Ellis, “ Solid rocket motor nozzles”, NASA SP 8115,

June, 1975

42. Woodberry, "Flexible joints for thrust vector controls", AIAA-75-

1221, October, 1975

43. Walker, “Development and demonstration of an omni-axial

flexible seal movable nozzle for thrust vector control”, AFRPL-TR-

67196.

44. Gajbir Singh and Rao, G.V., “New formulas for design of flex

bearing”, Journal of Spacecraft, vol.30, No 6, 1991.

45. Donat James, "Solid Rocket Motor Nozzle Flex seal Design"

AIAA-1993-1122, AHS and ASEE, Aerospace Design Conference,

Irvine, CA; United States; 16-19 Feb. 1993.

46. Prins.W., Meyer.S., Cox.P., "Advanced Solid Rocket Motor Nozzle

Thrust Vector Control Flex seal Development Status", AIAA 92-

3553, AIAA/SAE/ASME/ASEE, 28th Joint Propulsion Conference

and Exhibit, July 6-8, 1992/Nashville, TN.

47. Shimon Shani, Shlomo Putter and Arie Peretz, "Development of a

high-performance flexible joint for thrust vector control"

AIAA-1995-3017, ASME, SAE, and ASEE, Joint Propulsion

Conference and Exhibit, 31st, San Diego, CA, July 10-12, 1995.

48. Michel Berdoyes, Max Calabro, "The French Deterrent Force

SRMs: Genesis of Flex seals", AIAA-2008-5270, 44th

195


Exhibit, Hartford, CT, July 21-23, 2008.

49. Michel Berdoyes , “SRM nozzle design breakthroughs with

advanced composite materials” , AIAA-1993-2009, 29th


Exhibit, Moneterey, CA, June 28-30, 1993.

50. Michel Berdoyes, “Advanced Technology SRM Nozzles. History

and Future”, AIAA-2006-4596, 42nd AIAA/ASME/SAE/ASEE

Joint Propulsion Conference and Exhibit, Sacramento, California,

July 9-12, 2006.

51. Michel Berdoyes, Bernard Broquere, Sylvie Loison, Martine

Dauchier, “Sustainable C2 Rayon-Based Carbon Cloth for the

Ariane 5 SRM Nozzle”, AIAA-2005-3795, 41st


Exhibit, Tucson, Arizona, July 10-13, 2005.

52. Steven Peake, Russell Ellis, Bernard Broquere, “Sustainable

Carbonized Rayon for SRM Nozzles”, AIAA-2007-5774, 43rd


Exhibit, Cincinnati, OH, July 8-11, 2007.

53. Hamke. R, Rade. J, Weldin. R, "Development and qualification of

a STAR 48 rocket motor with thrust vector control", AIAA-1992-

3552, SAE, ASME, and ASEE, Joint Propulsion Conference and

Exhibit, 28th, Nashville, TN, July 6-8, 1992.

196

54. Mcgrath. D. “The history of Thiokol STAR motor missions”, AIAA-

1995-3129, ASME, SAE, and ASEE, Joint Propulsion Conference

and Exhibit, 31st, San Diego, CA, July 10-12, 1995.

55. Mcgrath.D, “Star Motors With Movable Nozzles” ,AIAA-1995-

3020, ASME, SAE, and ASEE, Joint Propulsion Conference and

Exhibit, 31st, San Diego, CA, July 10-12, 1995.

56. Thomas Rudman, James McKinnis , Lyn Van Winkle, Jay Friant,

“Titan IVB Launch Vehicle and Propulsion Systems”, AIAA-2006-

4359, 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference

and Exhibit, Sacramento, California, July 9-12, 2006.

57. Thomas Rudman, "Titan IVB, SRMU and Centaur propulsion

systems", AIAA-1998-3194, AIAA, ASME, SAE, ASEE Joint

Propulsion Conference and Exhibit, 34th, Cleveland, OH, July 13-

15, 1998

58. Jeffrey. O. Foote., “Titan IV Solid Rocket Motor Upgrade Program

at Alliant Techsystems Inc”, AIAA-1997-2991,



59. Chang, I-Shih, Patel, N. R., Yang, S., “Titan IV motor failure and

redesign analyses”, Journal of spacecraft and rockets 1995,

Vol.32, No.4, pp - 612-618.

60. Chang, I.-S., Patel, N. R., ”Titan IV SRMU anomaly and redesign

analyses”, AIAA-1994-3284, ASME, SAE, and ASEE, Joint

197

Propulsion Conference and Exhibit, 30th, Indianapolis, IN, June

27-29, 1994.

61. Wilson, W. G, Anderson, J. M , “Titan IV SRMU PQM-1 overview”,

AIAA-1992-3819, SAE, ASME, and ASEE, Joint Propulsion

Conference and Exhibit, 28th, Nashville, TN, July 6-8, 1992.

62. Didier Boury, Jacques Rey, Alain Cronier, Philippe Greco, G.

Chounet, “Rubber Materials and Solid Propulsion: General

Overview & Technical Challenges”, AIAA-2005-3609, 41st


Exhibit, Tucson, Arizona, July 10-13, 2005.

63. Larrieu. J. M, "Preliminary design procedure of solid rocket

motors at Societe Europeenne de Propulsion (S.E.P.)", AIAA-1996-

2902, ASME, SAE, and ASEE, Joint Propulsion Conference and

Exhibit, 32nd, Lake Buena Vista, FL, July 1-3, 1996.

64. Calabro, Max, Thepenier, Jean, "Large SRBs for future

launchers", AIAA-1997-2869, AIAA/ASME/SAE/ASEE Joint

Propulsion Conference and Exhibit, 33rd, Seattle, WA, July 6-9,

1997.

65. Calabro, Max, Perret, Jean, “History of solid propellant rocket

motors at Aerospatiale”, AIAA-1992-3615, SAE, ASME, and

ASEE, Joint Propulsion Conference and Exhibit, 28th, Nashville,

TN, July 6-8, 1992.

66. Didier Boury, "P80 Nozzle Development & Qualification

Synthesis", AIAA-2008-4968, 44th AIAA/ASME/SAE/ASEE Joint

198

Propulsion Conference and Exhibit, Hartford, CT, July 21-23,

2008.

67. Richard Fawcett, "Advanced 3rd Stage (A3S) Carbon-Carbon Exit

Cone", AIAA-2008-4888, 44th AIAA/ASME/SAE/ASEE Joint

Propulsion Conference and Exhibit, Hartford, CT, July 21-23,

2008.

68. Wilson. Johnson, "Dual Flex - A low horsepower flexible seal

nozzle", AIAA-1971-749.

69. Jonathan W. Wilson, Wendell O. Johnson and Philip C.

Sottosanti, ”Dual Flex—A Low Horsepower Flexible Seal Nozzle”,

Journal of Spacecraft and Rockets 1972, Vol.9, No.8, pp-567-568

70. Kearney.W.J, Moss.J.D, "Advanced Solid Rocket Motor nozzle

development status", AIAA-1993-2596.

71. Kirby, D. C, "Solid rocket motor thrust vector control system

selection" , AIAA-1964-230, American Institute of Aeronautics

and Astronautics, Annual Meeting, 1st, Washington, D.C., Jun

29- Jul 2, 1964.

72. Gaffin.R. D, "Space Shuttle Solid Rocket booster nozzle flexible

seal pivot point dynamics", AIAA-1977-986, American Institute of


Engineers, Propulsion Conference, 13th, Orlando, July 11-13,

1977.

199

73. Jae-Seok Yoo, “First Korea Space Launch Vehicle Kick Motor

Movable Nozzle Motion”, Journal of Spacecraft and Rockets 2010,

0022-4650 vol.47 no.1, pp - 153-168.

74. Eric Gautronneau, M Cutroni, “VEGA Program - The P80 FW

SRM Nozzle”, AIAA-2004-4219, 40th AIAA/ASME/SAE/ASEE

Joint Propulsion Conference and Exhibit, Fort Lauderdale,

Florida, July 11-14, 2004.

75. Gautronneau E, Boury D, Chevrollier A, Talamoni Y, “P80 nozzle

low cost technologies”, 57th International Astronautical Congress,

Valencia, Spain, Oct. 2-6, 2006.

76. O. Le Merrer, “Ariane 5 Solid Rocket Motor Nozzle Design”, AIAA

90-2083, AIAA/SAE/ASME/ASEE, 26th Joint Propulsion

Conference, Orlando, July 16-18, 1990.

77. Didier Boury, “ARIANE 5 SRM Nozzle Evolution”, 56th

International Astronautical Congress of the International

Astronautical Federation, the International Academy of

Astronautics, and the International Institute of Space Law,

Fukuoka, Japan, Oct. 17-21, 2005.

78. Didier Boury, M. Munoz, A. Albert, J.B. Lassalle, “Ariane 5 SRM

Nozzle Evolution”, AIAA-2002-4193, 38th


Exhibit, Indianapolis, Indiana, July 7-10, 2002.

79. Ellis, R. A., Berdoyes, M., “Supersonic splitline (SSSL) flex seal

nozzle technology evaluation program”, AIAA-1997-2721,

200



80. Gigou, Jacques, “Ariane-5 solid-propellant stage development”,

AIAA-1992-1656, Space Programs and Technologies Conference,

Huntsville, AL, Mar 24-27, 1992.

81. Wilbur C., Rafael. M. Felix., “The History of Large Solid Motor

Development in the United States and Repont”, AIAA-1994-3057,

ASME, SAE, and ASEE, Joint Propulsion Conference and Exhibit,

30th, Indianapolis, IN, June 27-29, 1994.

82. Marco Biagioni, Maurizio Cutroni , "P80 FW SRM - New

Technologies for Solid Rocket Motor - Status of Development",

AIAA-2004-4220 , 40th AIAA/ASME/SAE/ASEE Joint Propulsion

Conference and Exhibit, Fort Lauderdale, Florida, July 11-14,

2004.

83. Valanis.K.C., “ The strain energy function of a hyper elastic

material in terms of the extension ratio”, Journal of Applied

Physics, Vol 38, no 7, June 1967, pp 2997-3002

84. Ghosh.P, Asaha, Bohara.P.C., “Material property characterization

for finite element analysis of tyres”, Rubber World, January 2006,

pp 22-31.

85. Yeoh.O.H, “Some benchmark problems for FEA from torsional

behaviour of rubber”, Rubber Chemistry and Technology, Vol 76,

No 3, 2003, pp-1212-1227.

201

86. Sivaramakrishnan. R and Bhagawan.S.S., “Characterisation of

Natural Rubber Based Flex Nozzle Material for Solid Rocket

Motors”, IRMRA 15th Rubber Conference, pp 221 - 230

87. Mark Goldsborough, “Solid-State Thrust Vector Control Systems”,

AIAA-2006-4941, 42nd AIAA/ASME/SAE/ASEE Joint Propulsion

Conference and Exhibit, Sacramento, California, July 9-12, 2006.

88. Raziye Tekin, Özgür Atesoglu, Kemal Leblebicioglu, "Modeling and

Vertical Launch Analysis of an Aero- and Thrust Vector

Controlled Surface to Air Missile", AIAA-2010-7639, AIAA

Atmospheric Flight Mechanics Conference, Toronto, Ontario, Aug.

2-5, 2010.

89. Tiarn, Weihnurng, Cavalleri, Robert, "CFD evaluation of an

advanced thrust vector control concept", AIAA-1990-1900, SAE,

ASME, and ASEE, joint propulsion conference, 26th, Orlando, FL,

july 16-18, 1990.

90. Nagappa, R., “Development of HTPB propellant system for ISRO's

motors”, AIAA-1990-2331, SAE, ASME, and ASEE, Joint

Propulsion Conference, 26th, Orlando, FL, July 16-18, 1990.

91. Chapman, John S., Nix, Michael B., “Overview of the

manufacturing sequence of the Advanced Solid Rocket Motor “,


Huntsville, AL, Mar 24-27, 1992.

92. Carroll, G. R., Cox, H., “A missile flight control system using

boundary layer thrust vector control”, AIAA-1983-1149, SAE, and

202

ASME, Joint Propulsion Conference, 19th, Seattle, WA, June 27-

29, 1983.

93. Croopnick, S., “Digital autopilot for thrust vector control of the

Shuttle orbital maneuvering system” Journal of Guidance,

Control, and Dynamics 1983, 0731-5090 vol.6 no.6 ,pp - 436-

441.

94. Michael Garrison, Scott Steffan , " Thrust Vector Control (TVC)

System Architecture Trade Study Overview ", AIAA-2007-

5848,43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference

and Exhibit, Cincinnati, OH, July 8-11, 2007

95. Alexander A. McCool, Adas J. Verble Jr., and Jack H. Potter, ,

"Space Transportation System Solid Rocket Booster Thrust Vector

Control System", Journal of Spacecraft and Rockets 1980, Vol.17,

No.5 pp-407-412

96. Thomason, H. E., "Space Shuttle system solid rocket booster.

"AIAA-1973-606, ASME, and SAE, Joint Space Mission Planning

and Execution Meeting, Denver, Colo., July 10-12, 1973.

97. Counter, D. N., "Thrust vector control for the Space Shuttle Solid

Rocket Motor", AIAA-1975-1172 American Institute of


Engineers, Propulsion Conference, 11th, Anaheim, Calif., Sept

29-Oct 1, 1975.

98. Stanley Baksi , Eric Besnard , "Low Cost Thrust Vector Control

System Development for Small Launch Vehicles", AIAA-2003-

203

5246 , 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference

and Exhibit, Huntsville, Alabama, July 20-23, 2003

99. Uhrig.G ,Boury. D, "Large space solid rocket motors in Europe -

Past and future developments", AIAA-1998-3980,


Exhibit, 34th, Cleveland, OH, July 13-15, 1998.

100.Calabro, M. / Dufour, A. / Macaire, A., "Optimization of the

propulsion for multistage solid rocket motor launchers" Acta

Astronautica, 50 (4), p.201, Feb 2002

101.Umholtz, Philip D, "The history of solid rocket propulsion and

Aerojet", AIAA-1999-2927, AIAA/ASME/SAE/ASEE Joint

Propulsion Conference and Exhibit, 35th, Los Angeles, CA, June

20-24, 1999.

102. “Pioneers in Propulsion—A History of CSD”, AIAA-2010-6909,

46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and

Exhibit, Nashville, TN, July 25-28, 2010.

103.John Robinson, Russell Rhodes, "Propulsion Technology Lifecycle

Operational Analysis", AIAA-2010-6505, 46th


Exhibit, Nashville, TN, July 25-28, 2010.

104.Schade, C. C., "Pegasus, Taurus and glimpses of the future",


Huntsville, AL, Sept 25-27, 1990.

204

105. ASME Boiler pressure vessel code, Section VIII.

106.Cowan, J. R, Myers, W. N. "Design of high power

electromechanical actuator for thrust vector control ",AIAA-1991-

1849 ,SAE, ASME, and ASEE, Joint Propulsion Conference, 27th,

Sacramento, CA, June 24-26, 1991.

107.Cesare Carnevale, "Vega Electromechanical Thrust Vector Control

Development" , AIAA-2007-5812 43rd AIAA, ASME, SAE, ASEE

Joint Propulsion Conference and Exhibit, Cincinnati, OH, July 8-

11, 2007

108.Weir, Rae A, "Development and test of electromechanical

actuators for thrust vector control", AIAA-1993-2458

109. John. D. Anderson, “Internal Aerodynamics in Solid Rocket

Propulsion”, Research and Technology Organisation, France,

2004.

110.Alexander Blake, “Design of Mechanical Joints”, Marcel Dekker.

Inc, New York and Basel, 1985.

111.Schneider, R.W., and Waters, E.O., The Background of ASME

Code Case 1828: A simplified Model of Analyzing part B Flanges,

Journal of Pressure Vessel Technology, ASME, Vol.100, No.2, May

1978, pp.215-219

112.Schneider, R.W., and Waters, E.O., The Application of ASME

Code Case 1828, Journal of Pressure Vessel Technology, ASME,

Vol.101, No.1, February 1979, pp.87-94.

205

113.John H. Bickford, “An introduction to the design and behavior of

Bolted joints”, Marcel Dekker Inc, New York.

114.R.W.Schneider, “Flat Face Flanges with metal-to-metal contact

Beyond the Bolt circle”, Journal Engineering for power, 1968.

115. NASA RP-1228, “Fastener design Manual”.

116. Nagendranath.A., Rao.N.V.M., Ram Mohan.CH.V.,

Gupta.R.K.,”Large Diameter Rocket Motor Casing Joint Analysis”,

Aero Tech, 2008, National Seminar on ‘Recent Advances in

Aerospace Technologies, Maintenance and Optimization’,

November 14-15, 2008

117.Wong E.Y. Design, Fabrication and test of omni directional

flexible seals for thrust vector control of large solid rocket motors,

NASA CR-72889.

118. Ram Mohan.CH.V., Ramanathan.J., Gupta.A.V.S.S.K.S., Sathish

Kumar., " Characterization of materials used for flex bearings of

large solid rocket motors", Defence Science Journal, Vol.61, No.3,

May-2011.

119. Mary C. Boyce, Ellen. M. Arruda, “Constitutive models of Rubber

Elasticity: A review”, Rubber Chemistry and Technology, Vol 73,

No 3, 2000, pp-504-523

120. Seibert.D.J, Schoche.N, “Direct comparison of some recent

rubber elasticity models” Rubber Chemistry and Technology, Vol

73, No 2, 2000, pp-366-384

206

121. Amin.A.F.M.S, Wiraguna.S.I, Bhuiyan.A.R, Okui.Y, " Hyper

elasticity model for finite element analysis of natural and high

damping rubbers in compression and shear", Journal of

engineering mechanics, Jan 2006, 54-64.

122. Li-Rong Wang and Zhen-Hua Lu, ”Modeling method of

constitutive law of rubber hyper elasticity based on finite element

simulations”, Rubber Chemistry and Technology, Vol.76, No 2,

2003, pp 271-285.

123. Pedro A.L.S. Martinsz, Renato M. Natal Jorgex, and Antonio J.M.

Ferreiray," Determination of Material Parameters for Different

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