Preston Layton Papers
Finding Guide
Boxes 61-68

 

Box 61  Princeton University Department of Aerospace and Mechanical Sciences (AMS) Reports

61-1	"The Design and Development of Rogowski Coil Probes for Measurement of Current Density Distribution in Plasma Pinch," Department of Aerospace and Mechanical Sciences, June 1965.
61-2	"The Movement of the Atmospheric Wind Profile," Robert F. Stengel, February 1968.
61-3	"Nuclear Rocket Systems and Mission Analysis Research: Preliminary Performance and Sensitivity Studies of the 750 Mwt Nuclear Rocket Engine," J.P. Lay ton, October 1,1970.
61-4	"Analytical Determination of the Adjoint Vector for Optimum Space Trajectories," P.M. Lion, June 1, 1970.
61-5	"Investigation About Some Impulsive Trajectories for Optimal Rendezvous," P. M. Lion, July 1970.
61-6	"An Analytical Solution for Constant-Thrust Optimal- Coast Minimum Propellant Space Trajectories," G.A. Hazelrigg, July 1970.
61-7	"Low Thrust Mission Analysis using an Analytical Trajectory Optimization Model," G.A. Hazelrigg, January 1970.
61-8	"Optimal Astronautical Guidance," A.L. Kornhauser, November 1970.
61-9	"Reliability Model of a Monopropellant Auxiliary Propulsion System," Joel S. Greenberg, June 25, 1971.
61-10	"Mathematical Model and Computer Code for the Analysis of Full Flow Cycle Nuclear Rocket Engine system Performance," M.D. Mintz, October 31, 1971.
61-11	"User's Guide for a Computer Code for the Analysis of Full Flow Cycle Nuclear Rocket Engine System," M.B. Silverman, January 18, 1972.
61-12	"Parameter Study of the Full Flow Cycle Nuclear Rocket Engine System Analysis Code," M.B. Silverman, January 18, 1972.
61-13	"Nuclear Rocket Engines Payload Performance Analysis Using Mission-Related Sensitivity Functions," R. Vichnevetsky, August 1, 1971.
61-14	"Mathematical Model for the Analysis of Small Nuclear Rocket Engine Performance," Jerry Grey, June 30, 1972.
61-15	"An Approach to Reliability Uncertainty and Risk Assessment of Space Systems," Joel S. Greenberg, June 6, 1972.
61-16	"Performance and Reliability Analysis of a Pluto Flyby Mission," George A. Hazelrigg, December 28, 1972.
61-17	"Plasma Propulsion systems," Arnold J. Kelly and Kenn E. Clark, September 1972.
61-18	"Analytical Basis for a Low-Power Dual-Mode Nuclear Rocket Engine Systems Analysis Code (NuROC 2C/SAC)," Jerry Grey, December 31, 1972.
61-19	"Reliability, Uncertainty and Risk Analysis of Space Systems- A Methodology for Decision Making," Joel S. Greenberg, December 27, 1972.
61-20	"Economics of Standardized Nuclear Powered Spacecraft" Joel S. Greenberg, February 1, 1974.
61-21	"A Methodology for Decision Making," Joel S. Greenberg, December 31, 1974.

 

Box 62 Princeton University Department of Aerospace and Mechanical Sciences (AMS) Reports

62-1	"Semi-Annual Progress Report on Nuclear Fusion Systems Analysis Research," R. K. Weather wax, July 1- December 31, 1974.
62-2	"Research on the Analysis of Nuclear Spacecraft and Special Nuclear Reactor Applications," J. S. Greenberg, July 1- December 31, 1974.
62-3	"Preliminary Analysis of Mini-Cavity Plasma Fission Reactors for Dual-Mode Propulsion Systems," Stanley Chow, October 1975.
62-4	"Mathematical Model for the Preliminary Analysis of Dual-Mode Space Nuclear Fission Solid Core Power and Propulsion Systems," Jerry Grey and Stanley Chow, June 30,1976.
62-5	"Mathematical Model for the Preliminary Analysis of Dual-Mode Space Nuclear Fission Solid Core Power and Propulsion Systems," The Aerospace Systems Laboratory, February 20, 1973.
62-6	"Computer Code and Users' Guide for the Preliminary Analysis of Dual-Mode Space Nuclear Fission Solid Core Power and Propulsion Systems," R. A. Nichols, June 30,1976.
62-7	"Parameter Study of Dual-Mode Space Nuclear Fission Solid Core Power and Propulsion Systems," William W. Smith, September 13, 1976.
62-8	"Nuclear Fusion Systems Analysis Research," R. K. Weatherwax, December 31, 1975.
62-9	"Economic Comparison of Fusion Power Alternatives," Joel S. Greenberg, October 31, 1975.
62-10	"Research on the Problem of Efficient R&T Program Formulation Under Conditions of Uncertainty and Risk," J. S. Greenberg, April 30, 1976.
62-11	"Economic Impact of New Technology on Domestic Satellite Communications," Volume I, Joel S. Greenberg, March 31, 1976.
62-12	"Economic Impact of New Technology on Domestic Satellite Communications," Volume II, Joel S. Greenberg, March 31, 1976.
62-13	"A Survey of Nuclear Fission Reactors for Space Power and Propulsion Applications," Jerry Grey and J. P. Lay ton, September 30, 1976.

 

Box 63 The Aerospace Systems Laboratory, Princeton University ASAR Memos

63- 1	"Record of Meeting on Nuclear Rocket system Analysis," Robert Vichnevetsky, February 8, 1967.
63-2	"Optimization Theory Course Notes," R. Vichnevetsky, January 1970.
63- 3	"Optimal Planetocentric High Thrust/Low Thrust Flight Equations," R. Vichnevetsky, September 27, 1970.
63-4	"Space system Comparison and Evaluation- Some Basic Concepts with Emphasis on Reliability," Joel S. Greenberg, May 28, 1971.
63- 5	"Full Flow Nuclear Rocket Engine System Analysis," Volume I, M. D. Mintz, August 19, 1971.
63-6	"Full Flow Nuclear Rocket Engine Systems Analysis," Volume II, M. D. Mintz, August 19, 1971.
63- 7	"Payload and Payload Sensitivity for a 300 MWt Class Nuclear Rocket Engine," R. Vichnevetsky, January 31,1972.
63- 8	"Effect of SNRE Parametric Variations Upon Payload for Escape Missions," R. Vichnevetsky, April 13, 1972.

Box 64  The Aerospace Systems Laboratory, Princeton University ASAR Memos

64-1	"Jupiter Orbiter/Probe Mission: A Spacecraft Packaging Concept for a Shuttle Launching," A. C. Gray, July 7,1972.
64-2	"Preliminary Discussion of a Reliability Program Plan for the Small Nuclear Rocket Engine," J. S. Greenberg and A. Sternberg, November 28, 1972.
64-3	"Research in Nuclear Fission Plasma Core Rocket Systems and Mission Analysis," S. Chow, July 10, 1973.
64-4	"Prospects for Nuclear Propulsion of Aircraft," J. P. Lay ton and J. Grey, January 31, 1975.
64-5	"Report on Rankine Cycle Parametric Analysis," Lih-Tah Wong, May 29, 1975.

 

Box 65   The Aerospace Systems Laboratory Princeton University STAR and MARS Memos

65-1	"Asmar Program Star Memos: A Primer on the Primer," April 21, 1967.
65-2	"Mars Memo #1: Lagrangian Multipliers," H. Handelsman.
65-3	"Mars Memo #2: Derivative of Switching Function...Orbit Transfer," H. Handelsman.
65-4	"Mars Memo #3: Useful Form of Wierstress Necessary... Problem," M. Handelsman.
65-5	"Mars Memo #4: Use of Weirstress Necessary... Orbit Transfer," M. Handelsman.
65-6	"Mars Memo #5: Some Notes on Talk by Prof. A. E. Bryson... Control Opt.," M. Handelsman.
65-7	"Mars Memo #6: Current Research Earth-Mars Round-Trip Trajectory Optimization Using Low-Thrust Propulsion," M. Handelsman, February 26, 1964.
65-8	"Mars Memo #7: Analytic Solutions to Variational...During Coast," M. Handelsman, March 6, 1964.
65-9	"Mars Memo #8: Suggestion for Checking An Iteration Program," M. Handelsman, March 12, 1964.
65-10	"Mars Memo #9: Variational Equations for Optimized... Coplanar Case," M. Handelsman, March 13, 1964.
65-11	"Mars Memo #10: Some Objectives in Trajectory... Mars Excursion," M. Handelsman, March 16, 1964.
65-12	"Mars Memo #11: Progress on Optimum One Way... Earth- Mars," M. Handelsman, March 25, 1964.
65-13	"Mars Memo #12: Differential Equations for the... Iteration Scheme," G. Hazelrigg, May 8, 1964.
65-14	"Mars Memo #13: Computation of Planetary Ephemeredes," G. A. Hazelrigg, May 20, 1964.
65-15	"Mars Memo #14: State of the Art Review," G. A.Hazelrigg, June 4, 1964.
65-16	"Mars Memo #15: Optimization of Interplanetary... Propulsion-I," M. Handelsman, June 8, 1964.
65-17	"Mars Memo #16: Normalization of Opt. Trajectory... Interplanetary Flight," M. Handelsman, November 16,1964.
65-18	"Mars Memo #17: The Behavior of the Switching Function... Flight Angle," M. Handelsman, November 25,1964.
65-19	"Mars Memo #18: calculation of Minimum-Fuel... Impulse Transfers," M. Handelsman, March 18, 1965.
65-20	"Mars Memo #19: Fixed-Time, Two-Impulse Interplanetary... Influence Concept," G. A. Hazelrigg, June 8, 1965.
65-21	"Mars Memo #20: Investigation of Double Minima... Orbital Transfer," S. M. Rocklin, August 23, 1965.
65-22	"Mars Memo #21a: Techniques of Analysis Planetary Escape... Part I," G. A. Hazelrigg, March 1, 1966.
65-23	"Mars Memo #21b: Techniques of Analysis Planetary Escape... Part II," S. M. Rocklin, June 16, 1966
65-24	"Mars Memo #22: Solution of the Equations... Matching Technique," G. A. Hazelrigg, February 28, 1966.
65-25	"Mars Memo #23: Record of Meeting on the Solar-Electric Propelled Spacecraft Mission Analysis," T. Edelbaum et al, March 9, 1966.
65-26	"Mars Memo #24: Preliminary Numerical Tests of... Iteration Technique," M. Handelsman, April 6, 1966.
65-27	"Mars Memo #25: Preliminary Results on Some... Between Circular Orbits," M. Handelsman, May 9, 1966.
65-28	"Mars Memo #27: Some Necessary Conditions for... Between Circular Orbits," M. Handelsman, October 13,1966.

 

Box 66  The Aerospace Systems Laboratory, Princeton University Student Thesis- Phd and MSE

66-1	"The Aerospace Systems Laboratory: A Mathematical Model and Computer Code for the Performance Analysis of Modular Nuclear Rocket Propelled Vehicles," Steven F. Cuspard, September 1972.
66-2	"A Mathematical Model and Computer Code for the Performance Analysis of Modular Nuclear Rocket Propelled Vehicles," Steven F. Cuspard, October 1975.
66-3	"Heat Transfer Measurements with Water Cooled Flush Diaphragm Pressure Transducers," Joseph Megerman, September 1967.
66-4	"Numerical Solutions of Optimal Fixed-Thrust Planetocentric Spiral Trajectories (Low Thrust)," Garwood W. Bacon, March 1970.
66-5	"Parametric Analysis of a Nuclear Powered High Length- to-Beam Captured Air Bubble Ship," David N. Seckinger, September 12, 1973.
66-6	"Parametric Analysis of a Nuclear Powered High Length- to-Beam Captured Air Bubble Ship," David N. Seckinger, September 12, 1973. (Hard Cover Copy).
66-7	"The optimization of Earth-Orbit Departure and Return Trajectories for Reusable Nuclear Rocket Vehicles," Wayne R. Spock, September

 

Box 67    The Aerospace Systems Laboratory, Princeton University Senior Thesis & Junior Independent Work.

67-1	"Preliminary Design of a Nuclear Powered Seaplane for Naval Command Applications," Todd R. Quackenbush, May 10, 1979.
67-2	"Configurationally Pumped Heat Pipe Radiators for Space Power Systems," D. Terrence Ball, May 1976.
67-3	"Nuclear Rocket Engine Sizing Analysis," Michael J.Flynn, December 1965.
67-4	"An Analysis of the Turboprop Aircraft Engine with Regard to Engine, Cycle, Propeller, and Regeneration, " Edward F. Wroe, Fall Term, 1968.
67-5	"An Introductory Study of Some Characteristics of Nuclear Rockets In Space Shuttles," Ralph W.H. Lim, January 15, 1973.
67-6	"The Chemical Stage of a Nuclear propulsion System," R. Dennis Macaleer, January 20, 1971.
67-7	"A Detailed investigation of the Ram-Jet Powered: Supersonic and Hypersonic Flight Vehicle," Phillip E.Griffin, January 13, 1969.
67-8	"A Model for an RTG Power System for a Spacecraft to the Outer Planets," Ralph W.H. Lim, June 1974.
67-9	"Proposed Space Test of A 25 kWe Zirconium Hydride Reactor with a Bray ton Cycle Power Conversion System," Robert W. Klein, May 1976.
67-10	"Launch Vehicles for Unmanned Solar System Exploration, 1970-1985," John Kerr.
67-11	"Aerospace Propulsion System and Mission Analysis: The Meaning of a Heat Flow Experiment on Mars," Thomas C. Hanks, June 7, 1966.
67-12	"Proposed Space Test of a 25 kWe Zirconium Hydride Reactor with a Bray ton Cycle Power Conversion System," Robert W. Klein, May 1976.
67-13	"An Experiment in Arc Plasma Jet Diagnosis," Lynn Robert Anderson, May 1965.
67-14	"An Analysis of the Turboprop Aircraft Engine with Regard to Engine Cycle, Propeller, and Regeneration," Edward F. Wroe, Fall Term 1968.
67-15	"Bray ton Power Conversion System for Space Applications," Lih-Tah Wong, April 23, 1976.
67-16	"Solar Flare Radiation Prediction to 1995," Edward Jay Sarton, April 26, 1967.
67-17	"Aerospace systems and Mission Analysis Research: Performance Analysis of the Solid Core Nuclear Rocket 1975-1985," Michael J. Flynn, December 30, 1966.
67-18	"A Model for an RTG Power System for a Spacecraft to the Outer Planets," Ralph W.H. Lim, June 1974.
67-19	"Application of the Initial QPT System Model to a Computer Analysis," Dennis E. Ludwig, September 7,1971.
67-20	"A Detailed Investigation of the RAM-Jet Powered Supersonic and Hypersonic Flight Vehicle," Phillip E.Griffin, January 13, 1969.
67-21	"Design of am Axisymmetric Supersonic Nozzle for Propulsion Testing," victor Lyman, June 30, 1965.
67-22	"A Primary Jupiter Orbiter: A Design Project," R.D. Fox, C.A. Nafziger, and V.L. Pell, Senior Thesis 1967.
67-23	"Investigations about Some Impulsive Trajectories for Optimal Rendezvous (vacant, circular, coplanar terminals)," J.P. Peltier.
67-24	"Launch Vehicles for Unmanned Solar System Exploration, 1970-1985," J. Kerr, Senior Thesis.
67-25	"The Meaning of a Heat Flow Experiment on Mars," Thomas C. Hanks, April 15, 1966.
67-26	"Study of a Small Solar-Electric Spacecraft," Franklin H. Moss, June 1971.
67-27	"High Performance Liquid Propellant Chemical Rocket Stage Analysis," R. Dennis Macaleer, May 24, 1971.
67-28	"Bray ton Cycle Conversion System for Initial Space Applications," Lih-Tah Wong, May 7, 1976.
67-29	"Configurationally Pumped Heat Pipe Radiators for Space Power Systems," D. Terrence Ball, Thesis, May 1976.
67-30	"Configurationally Pumped Heat Pipe Radiators for Space Power Systems," D. Terrence Ball, Thesis, May 1976.
67-31	"Design of an Axisymmetric Supersonic Nozzle for Propulsion Testing," victor Lyman, Thesis, June 30,1965.
67-32	"TRSYS-A Heliocentric Transfer Program Framework," Thomas R. Armstrong, Thesis, May 6, 1966.

Box 68   Soviet Space Books and Other Publications

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