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138
REFERENCES
1. C. D. Pengelley, Curtiss- Wright Corporation., “Ground Vibration
Tests” Journal Of The Aeronautical Sciences, Vol 9, No. 13,Nov
1942.
2. John W Miles., “On Structural Fatigue under Random Loading”,
Journal of the Aeronautical Science, pp753-762, Nov.1954
3. Crede, Charles E., “Concepts and Trends in Simulation,” Shock
and Vibration Bulletin 23, 1956.
4. McIntosh, W. C. and Granick, Neal, “Experiments in Random
Vibration,” Shock and Vibration Bulletin 23, 1956.
5. Noonan, Edward F., “Environmental Vibration Testing for
Shipboard Equipment,” Shock and Vibration Bulletin 23, 1956.
6. Hansen, W. O., “A Novel High- and Low-Temperature Horizontal-
Vibration Test Fixture,” Shock and Vibration Bulletin 25, 1956.
7. Armstrong, J. H., “Evaluating the Validity of Shock Simulations,”
Shock and Vibration Bulletin 23, 1956.
8. Morrow, C. T., “Some Special Considerations in Shock and
Vibration Testing,” Shock and Vibration Bulletin 23, 1956.
9. Booth, Galt B., “Introduction to Random Vibration: The Natural
Environment and Its Simulation,” Shock and Vibration Bulletin 23,
1956.
10. Wimpey, J. L., “Acceleration Spectral Density Spectrum,” Shock
139
and Vibration Bulletin 23, 1956.
11. Robbins, John, “Development of a White-Noise Vibration Test for
Electron Tubes,” Shock and Vibration Bulletin 23, 1956.
12. Wohl, R. J. and Schnee, M., “Impulse vs Steady-State Excitation in
the Evaluation of Electron Tubes,” Shock and Vibration Bulletin
23, 1956.
13. Warren, Raymond W., “Simulating and Controlling Response of a
Fuse Package,” Shock and Vibration Bulletin 23, 1956.
14. Yorgiadis, Alexander, “Acceleration Waveforms of Some Commonly
Used Mechanical Vibration Tables,” Shock and Vibration Bulletin
23, 1956.
15. Brown, E. H. and McClintock, R. M., “Vibration Testing Machines
in the One to Twenty Ton Load Range for Simulation of Transport
Conditions on Cryogenic Equipment and Missiles,” Shock and
Vibration Bulletin 23, 1956.
16. Barnes, W. P. and Mock, D. L., “Development of Vibrators for
Improved Simulation of Real Vibration Environment,” Shock and
Vibration Bulletin 23, 1956.
17. Edelman, Seymour, Jones, Earle, and Smith, Ernest R., “Barium
Titanate Vibrators,” Shock and Vibration Bulletin 23, 1956.
18. Blake, R. E., “The Need to Control the Output Impedance of
Vibration and Shock Machines,” Shock and Vibration Bulletin 23,
1956.
140
19. Mead, R. F., “Laboratory Simulation of Underwater Explosions,”
Shock and Vibration Bulletin 23, 1956
20. Gareau, R., “Development of a Heavy-Weight (2 to 20 ton) Shock
Testing Machine,” Shock and Vibration Bulletin 23, 1956.
21. Westgate, H. E., “A New 300-foot Universal Drop Tower,” Shock
and Vibration Bulletin 23, 1956.
22. Ottestad, J. B., “The HYGE Actuator in Shock Testing,” Shock and
Vibration Bulletin 23, 1956.
23. Sanders, S. P., “Pneumatic-Hydraulic Impactors for Producing
Controlled Acceleration,” Shock and Vibration Bulletin 23, 1956.
24. Shatz, G. W., “A Step Function Acceleration Machine for Light-
Weight Test Specimens,” Shock and Vibration Bulletin 23, 1956.
25. Jones, Earle, Edelman, Seymour, and Smith, Ernest R., “Small
Vibration Pickups,” Shock and Vibration Bulletin 23, 1956.
26. Meyer, D. D., “Direct Reading Probability Meter,” Shock and
Vibration Bulletin 23, 1956.
27. Upham, J. and Dranetz, A., “A Tape Recording Accelerometer for
Laboratory Playback, Analysis and Simulation,” Shock and
Vibration Bulletin 23, 1956.
28. Kroeger,R.C & Hasslaber,G.J., “ The relationship of measured
vibration data to specification criteria”, Shock and Vibration
Bulletin,1962, 31(2),49-63
141
29. David W. Gross and George Kachadourian., “ Simulation of In
flight lateral bending modes for Electrodynamic shaker testing”,
AIAA1963-1035
30. Potter, R. C., and Crocker, M. J., “Acoustic prediction methods for
rocket engines, including the effects of clustered engines and
deflected exhaust flow”, NASA CR-566, 1966.
31. Bies, D. A., “A review of flight and wind tunnel measurements of
boundary layer pressure fluctuations and induced structural
response”, NASA CR-626, May 1966.
32. Von Pragenau, George L., “Free flight Simulated on ground with
Apollo Saturn V Space Vehicle”, AIAA/JACC Guidance and
Conference, Seattle, WA, Aug 15016, 1966.
33. Lyon, R. H., “Random Noise and Vibration in Space Vehicles”,
Monograph SVM-1, Shock and Vibration Info. Anal. Ctr, 1967.
34. R. T. Spencer, “Development of a facility for remote vibration
testing of components while using hazardous cryogens”, AIAA-
1967-278
35. Sperling, F and Garba, J. A., “A treatise on the surveyer lunar
landing dynamics, and an evaluation of pertinent telemetry data
returned by surveyer I”, JPL TR 2- 1035, Jet Propulsion Lab,
Pasadena, CA, 1967.
36. Richards, E. J and Clarkson, B. L., “Jet and Rocket Noise”, Ch. 7,
Noise and Acoustic Fatigue in Aeronautics (Richards, E. J., and
142
Mead, D. J., Ed.), Wiley, NY, 1968.
37. Cockburn, J. A and Jolly, A. C., “Structural-Acoustic Response,
Noise Transmission Losses and Interior Noise Levels of an Aircraft
Fuselage Excited by Random Pressure Fields”, AFFDL-TR-68-2,
1968.
38. Lowson, M. V., “Prediction of boundary layer pressure
fluctuations”, AFFDL-TR-67- 167, Apr. 1968.
39. T.D.Scarton., “Development of Impedance Simulation Fixtures for
Spacecraft Vibration Tests”, NASA CR-1351,1969.
40. Goldman, R. L., “Transient Loads from Thrust Excitations”, NASA
SP-8030, 1969.
41. Himelbalau. H,C.Fuller and T.Scarton., “Assessment of Space
Vehicle Aero acoustic Vibration prediction, ”NASA CR 1596, July
1970
42. Rubin, S., “Prevention of Coupled Structure-Propulsion Instability
(Pogo)”, NASA SP 8055, Oct. 1970.
43. Eldred, K. M., “Acoustic Loads Generated by the Propulsion
System,” NASA SP- 8072, June 1971.
44. Robertson, E., "Prediction of In-Flight Fluctuating Pressure
Environments Including Protuberance Induced Flow", NASA CR-
119947, 1971.
45. Klee,B.J.,Kimball,D.V and Tustin,W., “Vibration and test fixture
design”, pp 12-1-12-6, Tustin Institute of Technology, California,
143
1971.
46. Curtis, A.J, Tinling, N.J and Abstein.H.T., “Selection and
performance of Vibration tests”, The shock and Vibration Center,
Naval Research Lab, Washington,1971.
47. Trubert, M. R., “A Practical Approach to Spacecraft Structural
Dynamics Problems,” J. Spacecraft and Rockets, Vol. 9, No. 11, pp
818-824, Nov. 1972.
48. Foley, J. T., "Transportation Dynamic Events Survey", Report EDB-
A1354 (DOE/DOD Environmental Data Bank), Sandia
Corporation, Albuquerque, NM, 1973
49. Houbolt, J. C., “Atmospheric Turbulence”, AIAA J., Vol.11, No. 4,
pp 421-427, Apr. 1973.
50. George M.Hieber., “A Low Class Fixture Can Spoil A High Class
Vibration Test” Machine Design, Nov. 14, 1974.
51. Ungar, E. E., et al., "A Guide to Estimation of Aeroacoustic Loads
on Flight Vehicle Surfaces,” AFFDL-TR-76-91, Feb.1977.
52. Anon., "Transportation and Handling Loads", NASA SP-8077,
Sept.1977.
53. Piersol, A. G. and Rentz, P.E., “Experimental Studies of the Space
Shuttle Payload Acoustic Environment,” SAE Paper 770973, Nov.
1977.
54. Berkman H.R.., “Control Point Averaging for Large Specimen
Vibration”, Shock and Vibration Bulletin, vol 37,pp 75-88, 1978.
144
55. J. R. Tegart Martin Marietta Corporation, Denver, Colo. And J. C.
Aydelottt ., “Effect of Vibration on Retention Characteristics of
Screen Acquisition Systems” VOL. 16, NO 5, SEPT.-OCT.
1979,Article NO. 78-1030R, J. Spacecraft 319
56. Wayne Tustin., “Vibration, Shock and Intense Noise testing for
reliability” IEEE, Transactions on reliabiltity,Vol.R28-No.2, p129-
132, June 1979
57. Wilby, J. F., and Pope, L. D., “The Development of a Method for
Predicting the Noise Exposure of Payloads in the Space Shuttle
Orbiter Vehicle,” Shock and Vibration Bull., No. 49, Part 1, pp 1-
29, Sep. 1979.
58. Pope, L. D., Wilby, J. F., et al, "Space Shuttle Payload Bay Acoustic
Prediction Model,” NASA CR-159956, Vol. I-V, Mar. 1980.
59. El-Raheb, M., and Wagner, P., "Vibration of a Liquid with Free
Surface in a Spinning Spherical Tank", J. Sound and Vibration,
Vol 76, No.1, pp 83-93, Jan.1981.
60. Keegan, W. B., et al, "Payload Bay Acoustic and Vibration Data
From STS-1 Flight,” NASA GSFC DATE Rep. 002, June 1981.
61. Balendra, T., Ang, K. K., Paranasivan, P., and Lee, S. L., "Free
Vibration Analysis of Cylindrical Liquid Storage Tanks", Int. J.
Mech. Sci., Vol.24, No.1, pp.47 - 59, 1982.
62. Dougherty, N. S., Nesman, T. E., and Guest, S. H., "Shuttle SRB
Ignition Overpressure: Model Suppression Test Program and Flight
145
Results", Proc. 13th JANNAF Plume Technology Mtg, Apr. 1982.
63. D.L.Jensen., “Flight Control Frequency Response Testing of the
Shuttle Ascent Vehicle” Vol. 5, NO. 3, May-June 1982 J. Guidance
243 , AIAA 80-1751R
64. Fenwick, J. R., Jones, J. H., and Jewell, R. E., "Space Shuttle Main
Engine (SSME) Pogo Testing and Results", Shock and Vibration
Bulletin, No.52, Pt. 2, pp.1 - 20, 1982.
65. Modlin Thomas C,Jr.Zupp, Geaorge A.Jr., “Shuttle Structural
Dynamic Characteristics, the Analysis and Verification”, Space
Shuttle Technical Conference, Houston, Texas, June 1983
66. Tanner, C. S., "Shuttle Cargo Bay Vent Noise and its Effect on the
Generic Payload Specifications and Testing Methods", Proc.,
Shuttle Payload Dynamic Environments and Loads Prediction
Workshop, Vol.1, pp.303 - 332, Jet Propulsion Laboratory, Jan.
1984.
67. Ray, G. A., and Kaminsky, J. A., “A Correlation of Analysis and
Flight- Measured Space Shuttle Responses to the STS-2 Lift-Off
Environment,” Proc. Shuttle Payload Dynamic Environments and
Loads Prediction Workshop, pp 173-181, Jet Propulsion
Laboratory, Pasadena, CA, Jan. 1984.
68. Brodeur, S. J., “Comparison of Flight Data Versus Predictions for
Low Frequency Acceleration Loads on STS-3 / OSS-1
146
Instruments,” Proc. Shuttle Payload Dynamic Environments and
Loads Prediction Workshop, pp 183-203, Jet Propulsion Lab,
Pasadena, CA, Jan. 1984
69. Cho, A. C., Dougherty, N. S., and Guest, S. H., “Scale Model
Acoustic Test of SSV for VAFB,” Proc. Shuttle Payload Dynamic
Environments and Loads Prediction Workshop, pp 153-172, Jet
Propulsion Lab, Pasadena, CA, Jan. 1984.
70. Lee, Y. A., Henricks, W., et al, "Vibroacoustic Payload Environment
Prediction System (VAPEPS),” Vol. 1 to 5, NASA CR-166823, June
1984
71. G.D. Shepard., “On Anti-resonance with application to Control of
Structurals”, Proceedings of 3 rd IMAC, pp 523-526, 1985.
72. Wilby, J. F., and Piersol, A. G., "An Evaluation of the Space Shuttle
Vibration at the Payload Attachments During Liftoff", Astron Rep.
7072-01, Aug. 1986.
73. Michael J.Debreceni, William D.Lay, T.K.Kuo and Donald E.Jackle
Jr., “Design and development of a communications satellite
propellant tank,” AIAA 86-2749.
74. Kipp, R. J., and Bateman, V.1., "Analytical Estimation of Earth
Penetrator Structural Response and Comparison with Laboratory
Shock and Modal Test Data", Proc., 59th Shock and Vibration
Symp., Vol. IV, pp.133-144, 1988.
147
75. Johnston, J. D., “Payload Bay Atmospheric Vent Airflow Testing at
the Vibration and Acoustic Test Facility,” NASA TM 100460, Feb.
1988.
76. Smallwood,D.O ., “An Analytical study of a Vibration test method
Using External control of Acceleration and force”, Proceedings of
the Institute of Environmental Sciences, 35th annual technical
meeting, 1989, pp.263-271
77. Scharton, T., “Development of Dual Control Vibration Testing,”
Proceedings of the Institute of Environmental Sciences Annual
Meeting, pp 140-1 46, April 1990.
78. Smallwood, D. O., “Development of the Force Envelope for an
Acceleration/Force External Controlled Vibration Test,”
Proceedings of the 61 st Shock and Vibration Symposium, Vol. 1,
pp 95-104, October 1990
79. Scharton, T., “Force Specifications for External Dual Controlled
Vibration Test,” Proceedings of the 61st Shock and Vibration
Symposium, Vol. 1, pp 105-1 16, October 1990.
80. Chang KY, Frydman A.M., “Three dimensional Random Vibration
Testing Definition and Simulation” , Proceedings of the 36 th
Annual Technical Meeting of the Institute of Environmental
Sciences. Mount Prospect,IL: Institute of Environmental Sciences
and Technology”,1990
148
81. J. R. Rollins, R. K. Grove, J. D. Price, and J. A. Miller, “Component
Level Structural Testing Of Satellite Surface Tension Propellant
Tanks”, A1AA1990-2224
82. S.A.Palani Swami., “Evolution of Environmental Vibration test
specifications for ISRO Launch vehicles”, 41st Congress of the
International Astronautical federation, Oct.6-12,1990
83. Smallwood.D.O., “Development of the force envelope for an
acceleration/force controlled vibration test”, Proceedings of the 61st
shock and Vibration symposium ,pp 95-104, Oct 1990
84. Scharton,Terry D, “ Analysis of dual control vibration testing”
Institute of environmental sciences Annual meeting, San Diego,CA,
1990
85. Freeman M.T., “3-axis Vibration system simulates a real world”,
Test Engineering and Management, pp 10-14,Dec/Jan 1990-91
86. Justus, C. G., "Mars Global Reference Atmospheric Model for
Mission Planning and Analysis", J. Spacecraft and Rockets, Vol.28,
No.2, pp 216-221, 1991.
87. McInerny, S. A., "Characteristics and Predictions of Far-Field
Rocket Noise", Noise Control Engineering, Vol. 38, No. 1, pp 5 - 16,
Jan/Feb. 1992.
88. Bausch H.P, A.Franz, M.Lapin., “Simultaneous, Multi-axial
Vibration Testing in Six Degrees of Freedom.” Sound and
Vibration, pp 6-11, Nov.1992.
149
89. Beranek, L. L., and Ver, I. L., Ed., “Noise and Vibration Control
Engineering” Wiley, NY, 1992.
90. Blevins, R. D. Flow., “Induced Vibration”, Melbourne, FL, 2nd ed.,
1992.
91. Michael J, R.K.Grove, J.A. Miller and J D Price, “ Design and
qualification of the Eurostar 2000 Propellant tank” AIAA-92-3606
92. Scharton,Terry D, “ Force limited vibration testing at JPL” 14th
Aerospace testing seminar, EI Segundo, CA-1993
93. H.Troidl, U.Schildl: “ vibration tests on the Arian 5 Thrust Frame-A
Challenge due to Exceptional Mass and Size of the Test Article”;
ESA WPP-066, pp.207-213, 1993
94. Terry Scharton, “Vibration and Shock Test Control Techniques”
ITEA Journal September 1993
95. Kajiwara.I, Nagamatsu., “Optical Design of Optical Pick-up by
elimination of resonance peaks”, J.Vibration and Acoustics,
Vol.115, pp377-383, 1993.
96. Allan G. Piersol “Accelerated vibration testing” (Tustin Training
News Date: January 1993)
97. Scharton.D., “Vibration test force limits derived from frequency
shift method”, Jet Propulsion Laboratory, JPL internal
document,D-11455,1994
98. Jones, J. H., et al., "Acoustic, Overpressure and Unsteady Flow
Phenomena Associated with the Saturn Space Shuttle Systems: A
150
Review of Selected Issues", Symp. Acoustics and Dynamic
Environment of Space Transportation Systems, CNES/ONERA,
Chatillon, France, Feb. 1994.
99. David O.Smallwood., “The role of Force measurements in Advanced
Vibration test methods” SAND 94-2681-C, 13 th IMAC, Nashville,
Feb 13-16, 1994.
100. Himelblau, H., Piersol, A. G., Wise, J. H., and Grudvig, M. R.,
“Handbook for Dynamic Data Acquisition and Analysis,” IES-RP-
DTE012.1, Inst. Envir. Sc. Tech., Mount Prospect, IL, Mar. 1994.
101. Terry D. Scharton, Jet Propulsion Laboratory, California Institute
of Technology, Pasadena, California 91109, “Vibration-Test Force
Limits Derived from Frequency-Shift Method” Journal Of
Spacecraft And Rockets, Vol. 32, No. 2, March-April 1995
102. He.J and Li.Y.Q., “Relocation of anti-resonances of vibration
system by local structural change”, Int. J. Analytical and
Experimental modal Analysis,Vol.10, no.4,pp 224-235,1995
103. Scharton, T., „Vibration Test Force Limits Derived From Frequency
Shift Method,” AIAA, Journal of Spacecraft and Rockets, March-
April, 1995.
104. Davis.J.M., “Fitting Multi-axis Vibration Testing into a Small
Laboratory”, Test Engineering and Management, pp16-18, Aug-
Sept 1995.
151
105. Pratt, H.K., et al, “Space Shuttle System Acoustics and Shock Data
Book,” Rockwell Intern. Rep. SD 74-SH-0082B, Change Notice 3,
1995.
106. Kim , J.Y, Chang, S.J,Kim, D.Y and Jeong, W.B., “ A study on the
determination of Optimal reference spectrum for Random Vibration
Control in environmental vibration tests”, KSME Journal, Vol.10,
No.2, pp 246-254, 1996.
107. Michael J. Debreceni, William D.Lay , T.K.Kuo, Donald E,Jackle, “
Design and development of a communications satellite propellant
tank” AIAA 96-2749
108. Hall, W. J., "Vibration of Structures Induced by Ground Motions",
Ch. 24 in Shock and Vibration Handbook, 4th ed. (Ed. C. M.
Harris), McGraw-Hill, NY, 1996.
109. Davenport, A. G., "Vibration of Structures Induced by Winds", Ch.
29, Pt II in Shock and Vibration Handbook, 4th ed. (Ed. C. M.
Harris), McGraw-Hill, NY, 1996.
110. Dotson, K. W., and Tiwari, S. B., "Formulation and Analysis of
Launch Vehicle Maneuvering Loads", J. Spacecraft and Rockets,
Vol.33, No.6, pp.813-821, 1996.
111. Monteil, D., Guillaud, V., and Laurens, P., “Mastering the Effect of
Microvibrations on the Performances of Reconnaissance Satellites”,
Matra Marcone Space France Paper No. N96-13900, 1996
152
112. Salama, M.A, Kuo, C. P., Davis, G.L Rivellini, T. P and Sabahi, D.,
“Simulation of Impact Dynamics for Mars Landing”, AIAA
Dynamics Specialists Conf, Apr.1996.
113. K.Muhlbaur, U. Schildt., “Dynamic tests of Large ARIANE V
structures demonstrating the existing potential of testing future
Large Payloads”, Conference on Spacecraft Structures, materials
and Mechanical testing, Netherlands,27-29 March 1996(ESA SP-
386, June 1996)
114. Anon., “Payload Vibroacoustic Test Criteria,” NASA Engg Standard
NASA-STD- 7001, June 21, 1996.
115. NASA STD-7001., “Payload Vibroacoustic Test Criteria, National
Aeronautics and Space Administration Technical Standard, June
21, 1996.
116. Potter, R. C., and Crocker, M. J., “Acoustic Prediction Methods for
Rocket Engines, Including the Effects of Clustered Engines and
Deflected Exhaust Flow”, NASA CR - 566, Oct. 1966.
117. Bradford, L., and Manning, J. E., “Acoustic Blanket Effect on
Payload Acoustic Environment”, pp. 244-253, Proc., 42 ATM, Inst.
Envir. Sc. Tech., Mount Prospect, IL, 1996.
118. Milne, J. S., “General Environmental Verification for STS & ELV
Payloads, Subsystems, and Components,” NASA GSFC Doc. GEVS-
SE, Rev. A, 1996.
153
119. Harris, C. M., Ed., Shock and Vibration Handbook, 4th ed.,
McGraw-Hill, NY, 1996.
120. D.L.Edberg, P.Wilke, T.Davis, E.Fosness., “On the Design and
Testing of a Spacecraft Launch Vibration Isolation System(LVIS)”,
AIAA-97-1204
121. David O.Smallwood., “Characterizing Electrodynamic shakers”,
Proc of IES-1997
122. Etienne Balmes., “Garteur Group On Ground Vibration Testing”.
Results From The Test Of A Single Structure By 12 Laboratories In
Europe (proceedings of IMAC, February 1997)
123. T.D.Scharton., “Force Limited Vibration Testing Monograph,” NASA
RP-1403, May 1997.
124. D.B. worth, D.S.Kaufman., “Validation of force-limited Vibration
testing”, Aeropsace Testing Seminar, CA,Oct 14,1997
125. Meier.R.C., N.Otto, W. Pielimeir and V.Jeyabalan., “ The Ford
Vehicle Vibration Simulator for Subjective Testing” In proceedings
of the Noise and Vibration Conference, Traverse City, Society of
Automotive Engineers, Inc.1997.
126. Manning, J. E., "Statistical Modeling of Vibrating Systems," Ch. 78,
Encyclopedia of Acoustics, ed: M. J. Crocker, John Wiley & Sons,
Inc. 1997.
127. Kim J.Y, Yoon.E.J, Kim D.Y and Jeong.W.B., “An application of
sensitivity analysis of anti-resonance frequencies to structural
154
dynamic modification of Vibration Test Control”, Proceedings of 7th
Asia Pacific Vibration Conference, pp 436-441, 1997.
128. Kabe Alvar., “Design and Verification of Launch and Space
Vehicle”, AIAA -98-1718, April 1998
129. K.Y.Chang, T.D.Scharton., “Cassini Spacecraft Force Limited
Vibration Testing,” Sound and Vibration, March 1998,pp 16-20.
130. T.D.Scharton., “In-flight measurements of dynamic force”,
European Conference on Spacecraft, structures, materials and
mechanical testing, Braunschweig,GR,Nov.1998
131. Gaston Netter, Ulrich Renner, Michael Dreyer., “Design and
Verification of a Standard Surface Tension Propellant Tank”, AIAA
99-2178
132. Peter Avitable, ”Why You Can‟t Ignore Those Vibration Fixture
Resonances” Sound And Vibration, March 1999
133. Dotson, K. W., Womack, J.M., and Grosserode, P.J., “Structural
Dynamic Analysis of Solid Rocket Motor Resonant Burn,” AIAA 99-
1201, 40th AIAA/ASME/ASCE/ASC Structures, Structural
Dynamics, and Materials Conference, St. Louis, MO April 1999.
134. M.J.Vujcich, T.D.Scharton., “Combined Loads, Vibration, and
Modal Testing of the QuikSCAT Spacecraft” AIAA World Aviation
Conference, CA, Oct.1999, Paper No.1999-01-5551.
135. T.D.Scarton., “ Random Vibration Force measured on Hitch hiker
Canister on STS-96” SSP Structures Technical Interchange
155
meeting, NASA/GSFC, Nov.1999
136. Anon., "DOD Test Method Standard for Environmental Engineering
Considerations and Laboratory Test", MIL~STD-810F, Apr. 2000.
137. T.D.Scharton., “Force Limited Vibration Testing”, NASA Technical
Handbook,HDBK-7004, May 2000
138. M.E.Mcneils and T.D.Scarton., “Benefits of Force-limited Vibration
testing” 7th International Congress on Sound and Vibration, July
2000.
139. Hughes W.O, Mcneils and Goodnight TW., “Vibration testing of an
operating Stirling Converter”, NASA TM 2000-210526 , Nov.2000
140. K.Chang., “Force limit specifications v/s Design Limit loads in
vibration testing” European Conference on Spacecraft structures,
Materials and Mechanical Testing, 29 Nov.2000.
141. Kurng Y Chang, “ Deep Space 1 Spacecraft Vibration Qualification
Testing” journal of Sound and vibration, March-2001
142. T.Scharton., “Force Limits Measured on a Space Shuttle Flight,”
European Conference on Spacecraft Structures, Materials and
Mechanical Testing, Nov.2000, Paper No. ESA SP-468, March
2001.
143. Conor D.Johnson, Paul S. Wilke, Kenneth R. Darling., “Multi-axis
whole-spacecraft vibration isolation for small launch vehicles”,
SPIE Conference on Smart Structures and Materials, CA,pp 4331-
16, March 4-8, 2001
156
144. Tustin.W., “ Road frequencies contain all frequencies
simultaneously”, Test Engineering and Management, pp2-3, Aug-
Sept 2001.
145. Underwood M.A,T.Keller., “Recent system developments for Multi-
Actuator Vibration Control”, Sound and Vibration, PP 16-23, Oct
2001
146. Gyuhae Park, Eric Ruggeriero, Marion Sausse and Daniel
J.Inman., “Vibration Testing and Analysis of Inflatable Structures
using Smart Materials” ASME International Mechanical
Engineering Congress and Exposition, Nov 11-16, 2001, NY.
147. Whiteman W.E, M.Berman., “Inadequacies in Uniaxial stress
Screen Vibration Testing”, Journal of the Institute of
Environmental Sciences and Technology 44,4:20-23,Fall 2001.
148. Charles R ,Farrar, ScottW, ”Vibration –based structural damage
identification”, Phil.Trans.Royal Society,Londan.A-2001
149. Hank Caruso, “MIL-STD-810F, test method standard for
environmental engineering considerations and laboratory tests”,
Journal of the IEST,Summer-2001
150. George Fox Lang, Dave Synder., “Understanding the Physics of
Electrodynamic Shaker Performance”, Sound and Vibration,
Oct.2001
151. Manoj Kumar, T. Narasirnha Rao, K. Jagadisan and K. Jayathirtha
Rao “Tailoring of Vibration Test Specifications for a Flight Vehicle”-
157
Defense Science I, Vol. 52, N0.1, January- 2002
152. Lawrence Grasty, “ New Electromagnetic Shaker Technology”,
Journal of sound and vibration-March 2002
153. Terry D. Scharton, Jet Propulsion Laboratory, Pasadena, California
“Vibration and Acoustic Testing of Spacecraft” ,Sound and
Vibration -June 2002.
154. D.Michael McFarland, Darien L.Gipson, Alexander F.Vakakis,
Lawrence A.Bergman., “Characterization of an essentially non-
linear 2-DOF Vibration test apparatus” 15th ASCE Engineering
Mechanics Conference, NY,June 2-5,2002.
155. Rogerio Pirk, Wim Desmet, Bert Pluymers, Paul Sas, Luis C. S.
Goes “Vibro-acoustic Analysis of the Brazilian Vehicle Satellite
Launcher (VLS) fairing “,Proceedings of ISMA2002 - Volume V
156. Donald A. Barnes James T. Pontius, “Structural Qualification Of A
Spacecraft Payload Using Near-Resonance Sine Burst Testing”,
AIAA 2003-1452
157. Pierre Touzelet, “ Large Slip Table for Ariane 5 Satellite”, Hamburg,
Febraury-2003
158. Filip De Coninck, Wim Desmet, Paul Sas, David Vaes., “Multishine
shock and vibration testing using a High-frequency 6-DOF shaker
table” Tenth International Congress on Sound and Vibration, 7-10
July 2003.
158
159. Gyuhae Park, Marion Sausse, and Daniel J. Inman,Virginia
Polytechnic Institute and State University, Blacksburg, Virginia
24061-0261andJohn A. Main,University of Kentucky, Lexington,
Kentucky 40508 “Vibration Testing and Finite Element Analysis of
an Inflatable Structure”, AIAA JOURNAL, Vol. 41, No. 8, August
2003
160. Walter Tam, Mike Hersh, and Ian Ballinger, “ Hybrid propellant
tanks for space craft and launch vehicles”, AIAA 2003-4607
161. Vicente J. Suárez, Thomas W. Goodnight, William O. Hughesa,
Sergey Samorezov, “Vibration Modal Characterization of a Stirling
Converter via Base-Shake Excitation”, AIAA2003-6096.
162. J.H.Zhang,Y.H.Liu,J.Li, X.W.Zhu “The Study of Fixture for
Environmental Vibration Test of Space Structures” -54th
International Astronautical Congress of the International
Astronautical Federation, 29 Sept - 3 Oct 2003, Bremen, Germany
163. Andre Cote,St-Anne-de-Bellevue, Canada And Yvan Soucy,,
Canada “Force-Limited Vibration Complex Two-Degree of Freedom
System Method” AIAA JOURNAL,Vol. 42, No. 6, June 2004.
164. Jeannette Plante and Brandon Lee, Dynamic Range Corporation, “
Environmental conditions for space flight Hard ware-a Survey” for
the NASA Elecronic Parts and Packaging program-2004
165. John Steven Snyder , John R. Brophy., “Performance
Characterization and Vibration Testing of 30-cm Carbon-Carbon
159
Ion Optics”, AIAA-2004-3959
166. Jonathan Polaha, Nicole Meckel, and Benjamin Welander, Nils
Juhlin, Tom Haag., “Random and Sine-Spectrum Vibration Testing
of Pyrolytic Graphite Ion Optics” AIAA 2005-4395
167. Alexandre Popovitch., “ Multi shaker upgrade at ESTEC ESA” ,
Proceedings of the 22nd Aerospace Testing Seminar, the Aerospace
Corporation , Mar-2005
168. Dr S V Modak, BS Gandhare, “prediction of vibration
characteristics using structural Dynamic modification” IE(I)
Journal-MC,vol.86,july-2005
169. Otto Brunner., “Development of Large vibration Slip table” ,
Proceedings of the 22nd Space simulation conference, Baltimore,
October 2005.
170. Fabien Poncelet,” Optimal Design of Fixture for Vibration Testing of
Structures on Electro Dynamic Shaker”, 12th International
Congress on Sound and Vibration-2005
171. John Steven Snyder, Anita Sengupta, John S. Beatty, Michael R.
O.Connell., “Vibration Test and Analysis of a 20-kW-Class Ion
Engine” AIAA 2005-441
172. David W. Sleight, Troy O. Mann., “Finite element analysis and test
correlation of a 10-meter inflation deployed solar sail”,AIAA-2005-
2121.
160
173. John Steven Snyder, Anita Sengupta, John S. Beatty, Michael R.
O‟Connell, Brian Sullivan, Michael Collins, “Vibration Test and
Analysis of a 20-kW-Class Ion Engine” AIAA 2005-4412
174. H.Akesson, I.Gustavsson, L.Hakansson, I. Claesson., “Remote
Experimental Vibration Analysis of Mechanical Structures over the
Internet” American Society for Engineering Education Annual
Conference and Exposition, 2005.
175. Bart Peeters,Peter De Baets, Lorenzo Mosenich, Antonio Vecchio,
and Herman Van der Auweraer, Filip lambert, “Ground Vibration
Testing in the Aeroelastic Design and Certification of a Small
Composite Aircraft” AIAA 2005-2233
176. Suraj P. Rawal, and Alan R. Perry, Lockheed Martin Space
Systems, Littleton, Colorado 80125,John D. Williams, Paul J.
Wilbur, and D. Mark Laufer, Colorado State University, Fort
Collins, Colorado 80523,Wei Shih, AllComp, Inc., City of Industry,
California 91746 “Performance Evaluation of 8-cm-diam Ion Optics
Assemblies Fabricated from Carbon-Carbon Composites” Journal
of propulsion and power, Vol. 22, No. 3, May–June 2006
177. Y. Soucy, V. Dharanipathi, R. Sedaghati, “Investigation of Force-
Limited Vibration for Reduction of Over testing”, Journal Of
Spacecraft And Rockets, Vol. 43, No. 4, July–August 2006
178. Lien C. Yang, Lexter J. Granda, Thomas D. Klause, John H.
Seward “Dynamic Testing of Large Scale Destruct Charge
161
Assemblies”, AIAA 2006-4987
179. John Steven Snyder, Michael R. O‟Connell, Juan P. Fernandez,
“Vibration Test of a Breadboard Gimbal for the Next Ion Engine”
AIAA 2006-4665
180. Enrico Troiani, Davide Bruzzi, Stefano Gianotti, Paolo Tortora
“Almasat microsatellite structural analysis: finite elements
techniques, vibration tests and results correlation” IAC-06-B5.6.09
181. Charles D. Griffin, “Vibration Testing of the Pluto/New Horizons
Radioisotope Thermoelectric Generator” AIAA 2006-4030
182. R. Brett Williams and Rebekah Tanimoto, Andranik Simonyan and
Stephen Fuerstenau , “Vibration Characterization of Self-Cleaning
Solar Panels with Piezoceramic Actuation” AIAA 2007-1746
183. Natalie D. Spivey, Claudia Y. Herrera, Donald Freund, “Quiet Spike
TM Build-up Ground Vibration Testing Approach” AIAA 2007-1775
184. John Steven Snyder, John R. Anderson, “Environmental Testing of
the Next PM1 Ion Engine” AIAA 2007-5275
185. Philipp Behruzi, Charles Dodd, Gaston Netter., “Future propellant
management device concepts for restartable cryogenic upper
stages,” AIAA 2007-5498.
186. Joe Benton, Ian Ballinger, Donald E, Jaekle Jr, Michael F,
Osborn,”Design And Manufacture Of A Propellant Tank Assembly”
AIAA 2007-5559
162
187. Pierre Touzelet, Alexander Popovitch, Gaetan Piret, “ the ESTEC
New Quad head Expander” , proceedings of 6th international
Symposium on Environmental testing for space programme,
Noordwijk, The Netherlands, 12-14 june 2007
188. Ashok Joshi, D Ramakrishna , P M Mujumdar, Y Krishna.,
“Evolution of Vibration Testing Strategy Using Multi-Point
Excitation”, AIAA 2008-1853
189. D.Ravi Prasad and D.R.Seshu., “ A Study on Dynamic
Characteristics of structural materials using model analysis”,
Asian Journal of Civil Engineering ,Vol .9 , No 2 2008
190. G. Coppotelli, R. Rinaldi, and L. Balis Crema, “Structural Updating
of the VEGA-UCMEC FE Model Using Vibration Test Data” AIAA
2008-1850
191. Shun-fat Lung ,and Chan-gi Pak, “Updating the Finite Element
Model of the Aerostructures Test Wing Using Ground Vibration
Test Data” AIAA 2009-2528
192. Margaret L. Tuma, Ph.D., Bruce R. Askins,Donald J. Chenevert,
PhD., “Objectives and Progress on Ground Vibration Testing for the
Ares Launch Vehicles”, AIAA 2009-1154.
193. John D. Bernardin, Allen G .,“Mechanical Design and Dynamic
Testing of the IBEX-Hi Electrostatic Analyzer Spacecraft
Instrument”, AIAA 2009-2025
163
194. John Steven Snyder, John R. Anderson, Environmental Testing of
NASA‟s Evolutionary Xenon Thruster Prototype Model 1 Reworked
Ion Engine” Journal Of Propulsion And Power, Vol. 25, No. 1,
January–February 2009
195. Walter Gibbs, Justin Francis, Randy Spicer, and Kevin Schaeffer,
Michael R. O. Connell., “Vibration Testing of the Orbiting Carbon
Observatory (OCO) Spacecraft on a Passive Vibration Isolation
System” AIAA 2009-2635
196. John D. Bernardin, Allen G. Baca ,”Mechanical Design and
Dynamic Testing of the IBEX-Hi Electrostatic Analyzer Spacecraft
Instrument” AIAA- 2009-2025
197. Trevor Harrison., “Basic Fixture Design”, LDS Customer Training
Notes-2009
198. J.Santiago- prowald,ag noordwijk, and g.rodrigues., “qualification
of spacecraft equipment:early prediction of vibro acoustic
environment” journal of spacecraft and rockets, vol. 46,no.6,nov-
dec-2009
199. Walter Gibbs, Justin Francis, Randy Spicer and Kevin Schaeffer,
Michael R. O‟Connell., “Vibration Testing of the Orbiting Carbon
Observatory (OCO) Spacecraft on a Passive Vibration Isolation
System”, AIAA 2009-2635
200. Ashok Joshi,D Ramkrishna ,P M Mujumdar, ,Y Krishna,
“Identification of Multiple Input Forces in Vibration Testing of
164
Flight Vehicle Structures” AIAA 2010-2805
201. Sandro R. Rett, Airton Nabarrete, Mariano A. Arbelo, Luiz C. S.
Góes, Gustavo P. Guimarães., “Results of the GVT of the
Unmodified GARTEUR SM-AG19 Test bed in South America” AIAA
2010-2808
202. B.J.Klee, David V. Kimbal and Wayne Tustin., “ Vibration and
Shock Test Fixture Design”
203. Sheldon Levine., “ Vibration Test Fixture Theory and Practice” Aero
Nav Laboratories College point, New York
204. Dennis L. Kern, Terry D. Scharton “NASA handbook for spacecraft
structural dynamics testing”
205. John C. Forgrave , Kin F. Man , James M. Newell., “Acoustic and
Random Vibration Test Tailoring for Low-Cost Missions”
206. Philippe Fargette .,“Vibration Tests On Large Aircrafts”.
207. Keith Belvin, Harold H. Edighoffert., “Dynamic Analysis and
Experiment Methods for a Generic Space Station Model” , Journal
of Spacecraft, Vol. 24, No. 3.
208. Edgington F.M., “A three direction Vibration System”.
209. Kern D.Boatman, T.Scharton, Rentz., “Random Vibration Testing
of SIR-C Electronics Using Force Limited Techniques”, 63 rd Shock
and Vibration Bulletin
210. T.D.Scharton., “Force Specifications for Extreme Dual Controlled
165
Vibration tests”61st Shock and Vibration Bulletin.
211. David O.Smallwood., “Development of the Force Envelope for an
Acceleration/Force External Controlled Vibration Test” 61st Shock
and Vibration Bulletin.
212. Erwin Perl, Thinh Do, Alan Peterson and Jofn Welch,
“Environmental testing for launch and Space Vehicles”
213. Markku Juntunen, Kalle Vehvilainen, Kyosti Vakevainen, Kari
Ojala., “Development of shock and vibration test specifications for
telecommunication equipment in automotive environments,” Nokia
Research Center, Finland.
214. Schutt, Jeff., “ Vibration tests for real world”
215. Kurng Y.Chang, “Force limit specifications Vs Design limit loads in
Vibration Testing”
216. Margaret L Tuma, “ integrated vehicle ground vibration testing in
support of launch vehicle loads and controls analysis”
217. Jun Yeop KIM, “ An Experimental Approach for structural Dynamic
modification of the fixture in vibration test control”
218. Curt Nelson, “Vibration Test Evaluation-single axis, single shaker-
6DoF”