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Arrow Tech personnel have authored numerous technical publications.

Following is a partial list of those publications:

  1. Hathaway,W.H.,Hathaway,A.,Whyte,R.H.,Davis,B.S.,Brown,T.G.,Hepner,D.J., Combining Radar, YawSonde and On-Board Telemetry Data to Determine Aerodynamic Coeficients,51st Aeroballistic Range Association, Madrid, Spain, September 2000
  2. Abate,G.L.,Duckershein,R.P., Hathaway,W.H., Subsonic/Transonic Free FlightTests of a Generic Missile with Grid Fins, AFRL-MN-TR-2000-7014
  3. Kruggel,B.,Hathaway,W.H.,Asher, Experimental and Analytical Aerodynamicsof Missiles with Forward Flares, AFRL-MN-EG-TR-2000-,2000
  4. Hathaway,W.H., Winchenbach,G., Krieger,J., Free Flight Tests of 10 Degree Cones with a One Degree Articulation Angle, AIAA 99-0434, 1999
  5. Hathaway,W.H., Winchenbach,G.L., Krieger,J., Kline,R., Free Flight Aerodynamic Tests of the Navy 20mm Ramics Ammunition, AFRL-MN-EG-TR-1999-7009, 1999
  6. Berner,G., Chapman,G.,Hathaway,W.H., Winchenbach,G., Dynamic Stability Testing of Blunt Atmospheric Entry Configurations, ISL PU-354/99, 1999
  7. Berner,G., Fleck,V., Hathaway,W.H., Winchenbach,G., Aerodynamic Testing for Long Range Explosively Formed Penetrators, ISL PU-343/99, 1999
  8. Hathaway,W.H., Kruggle,B., Sigal,A., Whyte,R., High Angle of Attack Free Flight Missile Testing, AIAA-99-0435, 1999
  9. Erline,T.F., Hathaway,A.F., Dispersion Analysis of the XM881 Armor-Piercing Fin Stabilized Discarding Sabot (APFSDS) Projectile, ARL-MR-433, 1999
  10. Hathaway,W.H., Free Flight Aerodynamic Test of Bent 10 Degree Semi Angle Cones at Mach Numbers of 0.4 To 3.0, US Army, AFRL-MN-EG-1998-7036, 1998
  11. Dupuis,A.D., Hathaway,W.H., Aeroballistic Range Tests of the Basic Finner Reference Projectile at Supersonic Velocities, Canada, DREV-TM-9703, 1997
  12. Brown,T.G., Brandon,F.J., Harkins,T.E., Hathaway,W.H., Drag and Moment Coeficients Measured During Flight Testing of a 2.75 in. Rocket, AIAA-97-0634, 1997
  13. Abate,G.L., Hathaway,W.H., Whyte,R.L., Winchenbach,G.L., Aeroballistic Range Tests: 40mm PGU-9 B/B and PGU-9 B/C projectile Configurations, Wright Laboratory, WL-TR-1997-7005, 1997
  14. Hathaway,W.H., Howerton,W., Steinhoff,M, Whyte,R, Aerodynamic Data Base of the C130 Gunship 105mm M1 Projectile, Eglin AFB, WL-TR-7059, 1995
  15. Abate,G., Hathaway,W.H., Whyte,R., Winchenbach,G., Aeroballistic Range Tests: Scaled Models of the 105mm M1 Projectile and Modified Configurations, Wright Laboratory, WL-TR-95-7058, 1995
  16. Hathaway,W.H., Adelgren,R., HAVE DASH: Free Flight ARF Test Results, ARO-WH-002, January 1994.
  17. Howerton,C., Hathaway,W., HART 1993: Free Flight ARF Test Results, ARO-WH-94-001, January 1994.
  18. Abate,G., Hathaway,W.H., ARF-Alliant Test Program Aerodynamic Results, ARROW, February 1994.
  19. Swenson,M.W., Abate,G.L., Whyte,R.H., Aerodynamic Test and Analysis of Wrap-Around Fins at Supersonic Mach Numbers Utilizing Design of Experiments, AIAA-94-0200, Aerospace Sciences Mtg, January 1994.
  20. Whyte,R.H., Aerodynamic Coefficients Of The 20mm Cased Telescoped TP Projectile At Mach Numbers From 0. 7 To 4. 0, WL-TR-93-7065, September 1993.
  21. Whyte,R.H., Valentino,M., Aerodynamic Coefficients Of The 25-mmPGU-38/UHEI Projectile At Mach Numbers From 0. 7 To 3.2, WL-TR-93-7064, November 1992.
  22. Whyte,R.H., Hathaway,W.H., Valentino,M., Aerodynamic Coefficients of the 20-mm PGU-2 7/B and -28/B Projectiles at Mach 0. 7 to 3. 0, WL-TR-92-7069, July 1993.
  23. Abate,G., Hathaway,W.H., Aerodynamic Test Results: WAF - Base Cavity Test Model, ARROW, May 1993.
  24. Winchenbach,G.L., Stephens,M., Hathaway,W.H., Whyte,R.H., Aerodynamic Test Results: Have Slick Configurations, WL/MN-TR-91-78, September 1991.
  25. Whyte,R.H., Analysis of MK82 Bomb Trajectory Utilizing Yaw Sonde and ARFDAS Codes, ARROW-006-91, August 1991.
  26. Whyte,R.H., Hathaway,W.H., Aerodynamic Test Results: Single-Stage-To-Orbit (SSTO) Re-Entry Vehicle, ARROW-004-91, October 1991.
  27. Hathaway,W.H., Steinhoff,M., Whyte,R.H., Expert Systems For Ballistic Range Data Analysis, WL-TR-93-7073, October 1993.
  28. Burnett,J.R., Steams,B., Hathaway,W.H., PGU-31 APFSDS In-Bore Balloting Analysis, ARROW-012-92, August 1992.
  29. Hathaway,W.H., Aerodynamic Test Results: Fin Rod Configuration, ARROW-011-92, September 1992.
  30. Whyte,R.H., Hathaway,W.H., Whyte,S., Aerodynamic Test Results: Wrap-Around Fin Confgurations, ARROW-003-91, September 1991.
  31. G.Abate, W.H. Hathaway, Aerodynamic Test Results: Offset Fin Missile Confguration, AIAA Flight Mechanics Conference, August 1989.
  32. G.Abate, W.H. Hathaway and B.C. Wong, Aerodynamic Test Results: Scaled 105mm XM915/XM916, AFATL-TR-89-161, Sept. 1988
  33. Fischer, W.H. Hathaway, B.C. Wong, ARFDAS Users Manual, AFATL-TR-88-48, October 1988.
  34. Gates, W.H. Hathaway, R.H.Whyte, and B.C. Wong, Aerodynamic Test Results for the 20mm PGU-27/B and PGU-28/B Projectiles, AFATL-TR-86-96, Sept. 1986.
  35. Hathaway and R. Kittyle, Free Flight Aerodynamics of 20mm and 30mm Boomed Projectiles, AFATL-TR-86-93, August 1986.
  36. Whyte and E.F. Brown, Analysis of Free Flight Aerodynamic Range and Yaw Sonde Data for 155mm Projectiles M549A1 and XM785, ARLCD-TR-84027, March 1985.
  37. Burnett and R.H. Whyte, Free Flight Range Aerodynamic Test: May 1984 - 20mm MK149 APDS Projectile, GE Data Package, August 1984.
  38. Winchenbach, B.L. Uselton, W.H. Hathaway, R.M. Chelekis, Free-Flight and Wind Tunnel Data for a Generic Fighter Conf guration, Journal of Aircraft, Volume 21, January 1984.
  39. Whyte, R. Buff, D.A. Graham, Free-Flight Range Aerodynamic Test: Wraparound Fin Configuration at Subsonic and Transonic Mach Numbers, AFATL-TR-84-11, January 1984.
  40. Buff, G.L. Winchenbach, R.H. Whyte, Aerodynamics of Spin Stabilized Projectiles With Exterior Dimples, AIAA-83-2144, August 1983.
  41. Whyte, D.A. Graham, and G.L. Winchenbach, Aeroballistic Range Tests of 25mm Armor Piercing and Target Practice Projectiles, AFATL-TR-82-27, March 1982.
  42. Cobb, R.H. Whyte, P.K. Laird, The Effects of a Moving Component on the Motion of a 20-mm Projectile, AIAA Aerodynarnic Testing Conference, Colorado Springs, March 1980.
  43. Hathaway and R.H. Whyte, Aeroballistic Research Facility Free Flight Data Analysis Using The Maximum Likelihood Method, AFATL-TR-79-98, December 1979.
  44. Whyte, G.L. Winchenbach and W.H. Hathaway, Analysis of Free Flight Trajectory Data for a Complex Asymmetric Missile Configuration at Subsonic Mach Numbers, AIAA Flight Mechanics Conf., Boulder, Colorado, No. 79-1689, August 1979 (Journal of Guidance, Control, and Dynamics-Volume 4).
  45. Whyte, W.H. Hathaway, Aeroballistic Research Facility Data Analysis System, 30th Aeroballistic Range Association, Burlington, Vermont, September 1979.
  46. Hathaway, J.R. Burnett, R.H. Whyte, DREV A/B Ballistic Range Data Analysis System, Defence Research Establishment Valcartier, Canada, September 1979.
  47. Whyte, W.H. Hathaway, E.M. Friedman, Analysis of Free-Flight Transonic Range Data of the 155-mm M483A1 and XM795 Projectiles, ARLCD-CR-79016, August 1979.
  48. Hathaway, R.H. Whyte, K.K. Cobb, R.A. Pierro, Analysis of Aeroballistic Range Data of 20-mm Projectiles with a Moving Internal Component, ADPA Symposium on Ballistics, Monterey, California, October 1978.
  49. West, R.H. Whyte, Free-Flight and Wind Tunnel Test of a Missile Configuration at Subsonic and Transonic Mach Numbers with Angles of Attack up to 30 Degrees, 11th Navy Aeroballistic Symposium, Warminster, Pennsylvania, August 1978.
  50. Hathaway, R.H. Whyte, Free-Flight Data Analysis Using the Maximum Likelihood Technique, 28th Aeroballistic Range Association, Eglin Air Force Base, September 1977.
  51. Hathaway, R.H. Whyte, Aeroballistic Range Data Analysis for Non-symmetric Configurations, AFATL-TR-76-109, September 1976.
  52. Craver, W.H. Hathaway, R.H. Whyte, Yaw Sonde and Transonic Range Data Reductions on the 155-mm XM483 and Other Projectiles Utilizing Numerical Integration, Picatinny Arsenal TR-4872, November 1975.
  53. Hathaway, Analysis of the Free-Flight Aerodynamics on Non-symmetric Bodies from Ballistic Spark Range Data, Master's Thesis, University of Vermont, October 1975.
  54. Whyte, W.H. Hathaway, Aeroballistic Range Data Analysis for Free-Flight Reduction Computer Programs, Advanced Munitions Report, General Electric, September 1974.
  55. Whyte, W.H. Hathaway, Aeroballistic Range Data Reduction Technique Utilizing Numerical Integration, AFATL-TR-74-41, February 1974.
  56. Whyte, SPIN-73. An Updated Version of the Spinner Computer Program, Picatinny Arsenal TR-4588, November 1973.
  57. Whyte, W.H. Mermagen, A Method for Obtaining Aerodynamic Coefficients from Yaw Sonde and Radar Data, Journal of Spacecraft and Rockets, Volume 10, Number 6, June 1973.
  58. Whyte, R.C. Houghton, W.H. Hathaway, Description of Yaw Sonde Numerical Integration Data Reduction Computer Programs, Ballistic Research Laboratory, BRL-CR-280, May 1973.
  59. Whyte, A. Jeung, J.W. Bradley, Chapman-Kirk Reduction of Free-Flight Range Data to Obtain Nonlinear Aerodynamic Coefficients, Ballistic Research Laboratory, BRL-MR-2298, May 1973.
  60. Whyte, R.C. Houghton, User Manual for AEDC Range G Free-Flight Reduction Computer Programs, General Electric Report, TR-72APB550, October 1972.
  61. Kline, R.H. Whyte, Gazdayka, Aeroballistic Characteristics of the 5.58 Caliber, Spin Stabilized 105-mm XM380 Projectile, Picatinny Arsenal TR, June 1972.
  62. Whyte, R.C. Houghton, Reduction of Range and Yaw Sonde Data Using Numerical Integration Techniques, Ballistic Research Laboratory, BRL-CR-00400, September 1972.
  63. Whyte, R.C. Houghton, Input-Output Description of the Numerical Integration Programs ANGLES and HEEVE, General Electric TIS 72APB517, April 1972.
  64. Whyte, W.H. Hathaway, Reduction of Yaw Sonde and Position Time Radar Data by Numerical Integration, General Electric, Burlington, Vermont, 72APB506, January 1972.
  65. Whyte, A. Jeung, Aerodynamic Reduction of Free-Flight Transonic Range Data Utilizing Numerical Integration, General Electric TIS 7lAPB514, April 1971.
  66. Whyte, J.G. Beliveau, Reduction of 4.2 Inch Mortar Free-Flight Spark Range Data by Numerical Integration, Advanced Munitions Report, General Electric, Burlington, Vermont, August 1970.
  67. Whyte, J.G. Beliveau, Nonlinear Free-Flight Aerodynamic Reductions Using Angle of Attack Rate Data, General Electric Report TIS R69APB6, September 1969.
  68. Whyte, J.G. Beliveau, An Investigation of the Chapman-Kirk Free-Flight Data Reduction Technique, Advanced Munitions Report, General Electric, Burlington, Vermont, August 1969.
  69. Whyte, Aerodynamic Characteristics of the M374 81-mm Mortar Projectile, Picatinny Arsenal TR-3634, October 1968.
  70. Whyte, Aerodynamic Characteristics of the Picatinny Arsenal Supporting Research Vehicle, SRV-4, Picatinny Arsenal TR-3546, June 1967.
  71. Whyte, Subsonic and Supersonic Static Aerodynamics of the XM552, 30-mm Projectile (WECOM30), Picatinny Arsenal TR-3422, January 1967.
  72. Whyte, Effects of Boattail Angle on Aerodynamic Characteristics of the 175-mm M437 Projectile at Supersonic Mach Numbers, Picatinny Arsenal TR-1646, September 1965.
  73. Whyte,H.E., Hudgins, Effects of Nose Shape and Boattail Angle on Static Aerodynamic Characteristics of a 105-mm Shell at Mach 4.0, 4.5, and 5.0, Picatinny Arsenal TR-1248, January 1964.
  74. Whyte, Wind Tunnel Testing Facilities at Picatinny Arsenal, Picatinny Arsenal TR-1980, January 1963.

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