Clark, I., Hutchings, A., Tanner, C., Braun, R., "Supersonic Inflatable Aerodynamics Decelerators For Use On Future Robotic Missions To Mars," IEEEAC 1419, 2008 IEEE Aerospace Conference
March 2008, Big Sky, MT

Korzun, A., Cruz, J., Braun, R., "A Survey of Supersonic Retropropulsion Technology for Mars Entry, Descent and, Landing," IEEEAC 1246, 2008 IEEE Aerospace Conference
March 2008, Big Sky, MT

Lara, M., Russell, R., "Fast Design of Repeat Ground Track Orbits in High-Fidelity Geopotentials," A Symposium Honoring Byron Tapley's 50 Years of Contributions to Aerospace Education
February 2008, Austin, TX

Russell, R., Brinckerhoff, A.,  "Eccentric Orbits around Planetary Moons," AAS 08-181 2007-6020, AAS/AIAA Space Flight Mechanics Meeting
January 2008, Galveston, TX

Dubos, G., Saleh, J., Braun, R.,  "Technology Readiness Level, Schedule Risk and Slippage in Spacecraft Design: Date Analysis and Modeling," AIAA 2007-6020, Space 2007 Conference & Exposition
September 2007, Long Beach, CA

Dubos, G., Saleh, J.,  "Responsive Space: Concept Analysis, Critical Review, and Theoretical Framework," AIAA 2007-6015, Space 2007 Conference & Exposition 
September 2007, Long Beach, CA

Young, J., Wilhite, A.,  "A Value Proposition for Lunar Architectures Utilizing Propellant Re-supply Capabilities," IAC-07-A3.I.A.19, 58th International Astronautical Congress
September 2007, Hyderabad, India

Korzun, A., Braun, R.,  "Mars Gravity Biosatellite: Engineering, Science, and Education," IAC-07-A1.9-A2.7.05, 58th International Astronautical Congress
September 2007, Hyderabad, India

Alemany, K., Braun, R.,  "Design Space Pruning Techniques for Low-Thrust Multiple Asteroid Rendezvous Trajectory Design," AAS 07-348, AAS/AIAA Astrodynamics Specialist Conference
August 2007, Mackinac Island, MI

Young, J., Wilhite, A.,  "Development of a Lunar Architecture Simulation Environment for Evaluating the use of Propellant Re-supply," AIAA 2007-6620, AIAA Modeling and Simulation Technologies Conference and Exhibit
August 2007, Hilton Head, SC

Thompson, R., Krevor, Z., Young, D., Wilhite, A.,  "A Reduced Order Lunar Lander Model for Rapid Architecture Analysis," AIAA 2007-6623, AIAA Modeling and Simulation Technologies Conference and Exhibit
August 2007, Hilton Head, SC

Verges, A., Braun, R., "Evaluation of the Mars Pathfinder Parachute Drag Coefficient," 5th International Planetary Probe Workshop
June 2007, Bordeaux, France

Theisinger, J., Braun, R., "Hypersonic Entry Aeroshell Shape Optimization," 5th International Planetary Probe Workshop
June 2007, Bordeaux, France

Tanner, C., "Optimization of Earth Flight Test Trajectories to Qualify Parachutes for use on Mars," 5th International Planetary Probe Workshop
June 2007, Bordeaux, France

Thompson, R., Cliatt, L., Gruber, C., Steinfeldt, B., Sebastin, T., Wilson, J, "Design of an Entry System for Cargo Delivery to Mars," 5th International Planetary Probe Workshop
June 2007, Bordeaux, France

Krevor, Z., Wilhite, A., "Launch Vehicle Engine Selection Using Probabilistic Techniques," AIAA-2007-1963, 48th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics, and Materials Conference
April 2007, Honolulu, HI

Rohrschneider, R., Braun, R., "Aeroelastic Design Considerations of a Clamped Ballute for Titan Aerocapture," AIAA-2007-1850, 48th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics, and Materials Conference
April 2007, Honolulu, HI

Young, D., Wilhite, A., "A Resource Allocation Method for Achieving Optimal Reliability in a Lunar Architecture," AIAA-2007-1862, 48th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics, and Materials Conference
April 2007, Honolulu, HI

Alemany, K., Easter, R., Morse, E.,"Control Authority Analysis Applied to Lunar Outpost Deployment," IEEEAC 1090, 2007 IEEE Aerospace Conference
March 2007, Big Sky, MT

Alemany, K., Braun, R., "Survey of Global Optimization Methods for Low-Thrust, Multiple Asteroid Tour Missions," AAS 07-211, 2007 AAS/AIAA Space Flight Mechanics Meeting
January 2007, Sedona, Arizona

Young, D., Kokan, T., Ian, C., Tanner, C., Wilhite, A., "Lazarus: A SSTO Hypersonic Vehicle Concept Utilizing RBCC and HEDM Propulsion Technologies," AIAA-2006-8099, 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference
November 2006, Canberra, Australia

Tanner, C., Young, J., Thompson, R., Wilhite, A., "On-Orbit Propellant Re-supply Options for Mars Exploration Architectures," IAC-06-D1.1.01, 57th International Astronautical Congress
October 2006, Valencia, Spain

Kokan, T., Olds, J., "Characterizing High-Energy-Density Propellants for Space Propulsion Apllications," IAC-06-C4.P.10, 57th International Astronautical Congress
October 2006, Valencia, Spain

Krevor, Z., Wilhite, A., "Cost of Safety for Space Transportation," IAC-06-D1.1.08, 57th International Astronautical Congress
October 2006, Valencia, Spain

Young, D., Wilhite, A., "A Method for Allocating Reliability and Cost in a Lunar Exploration Architecture," IAC-06-D1.3.09, 57th International Astronautical Congress
October 2006, Valencia, Spain 

Young, J., Thompson, R., Wilhite, A., "Architecture Options for Propellant Re-supply of Lunar Exploration Elements," AIAA 2006-7237, AIAA Space 2006 Conference
September 2006, San Jose, CA.

Putnam, Z., Bairstow, S., Barton, G., Braun, R., "Improving Lunar Return Entry Footprints Using Enhanced Skip Trajectory Guidance," AIAA 2006-7438, AIAA Space 2006 Conference
September 2006, San Jose, CA.

Christian, J., Manyapu, K., Wells, G., Lafleur, J., Verges, A., Braun, R., "Sizing of an Entry, Descent, and Landing System for Human Mars Exploration,"                  AIAA 2006-7427, AIAA Space 2006 Conference
September 2006, San Jose, CA.

Alemany, K., Braun, R., Clark, I., Theisinger, J., Wells, G., "Mars Entry, Descent, and Landing Parametric Sizing and Design Space Visualization," AIAA 2006-6022, AIAA Astrodynamics Specialist Conference
August 2006, Keystone, CO.

Clark, I., Wells, G., Theisinger, J., Braun, R., "An Evaluation of Ballute Entry Systems for Lunar Return Missions," AIAA 2006-6276, AIAA Atmospheric Flight Mechanics Conference
August 2006, Keystone, CO.

Wooster, P., Braun, R., Ahn, J., Putnam, Z., "Trajectory Options for Human Mars Missions," AIAA 2006-6308, AIAA Astrodynamics Specialist Conference
August 2006, Keystone, CO.

Rohrschneider, R., Braun, R., "Static Aeroelastic Analysis of a Thin-Film Clamped Ballute for Titan Aerocapture,"  AA2006-1-33, 1st International ARA Days
May 2006, Arcachon, France.

Wells, G., Braun, R., An Entry Handbook for the Conceptual Design of Mars Missions AA2006-1-34, 1st International ARA Days
May 2006, Arcachon, France.

Masciarelli, J.P., J., Ware, J., Rohrschneider, R., Braun, R., Bartels, R., Moses, R., Hall, J., Ultra Lightweight Ballutes for Return to Earth from the Moon,
AIAA-2006-1698, 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
May 2006, Newport, RI.

Thompson, R., Olds, J.
System Architecture Modeling for technology portfolio Management using ATLAS
IEEE Aerospace Conference
March 2006, Big Sky, MT.

Alemany, K., Olds, J.
Probabilistic Cost, Risk, and Throughput Analysis of Lunar Transportation Architectures
IEEE Aerospace Conference
March 2006, Big Sky, MT.

Braun, R., Manning, R.
Challenges of Mars Entry, Descent and Landing
IEEE Aerospace Conference
March 2006, Big Sky, MT.

Prakash, R., Colby, L., Flaherty, K., Francis, S., Gunduz, M., Lafleur, J., Braun, R.
Design of a Long Endurance Titan VTOL System
IEEE Aerospace Conference
March 2006, Big Sky, MT.

Wells, G., Lafleur, J., Verges, A. Lewis, C., Christian, J., Manyapu, K., Braun, R.
Entry Descent and Landing Challenges of Human Mars Exploration
AAS 06-072, 29th AAS Guidance and Control Conference
February 2006, Breckenridge, CO.

Dec, J., Braun, R.
An Approximate Ablative Thermal Protection System Sizing Tool for Entry System Design
AIAA-2006-0780, AIAA Aerospace Sciences Conference
January 2006, Reno, NV

Young, D., Krevor, Z., Tanner, C., Thompson, R., Wilhite, A.
Crew Launch Vehicle (CLV) Independent Performance Evaluation

Alemany, K., Olds, J.
LASSO - Lunar Architecture Stochastic Simulator and Optimizer
AIAA 2005-6415, AIAA Modeling and Simulation Technology Conference and Exhibit
August 2005, San Francisco, CA.

Putnam, Z.R.; Braun, R.D.; Rohrschneider, R.R.; and Dec, J.A
Entry System Options for Human Return from the Moon and Mars
AIAA 2005-5915, 2005 AIAA Atmospheric Flight Mechanics Conference
August 2005, San Francisco, CA.

Colby, L.S.; Prakash, R; and Braun, R.D.
Nuclear Gas Turbine Propulsion System for Long Endurance Titan Exploration
AIAA 2005-4561, AIAA Joint Propulsion Conference
July 10-13, 2005, Tucson, AZ.

Kokan, T., Olds, J.
An Experimental and Analytical Study of High-Energy-Density propellants for Liquid Rocket Engines
AIAA-2005-4471, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
July 10-13, 2005, Tucson, AZ.

Young, D., Olds, J.
Artemis: A Reusable Excursion Vehicle Concept for Lunar Exploration
AIAA-2005-4010, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
July 10-13, 2005, Tucson, AZ.

Hutchinson, Jr., V., Olds, J., Alemany, K., Christian, J., Clark, I., and Crowley, J.
Tempest: Crew Exploration Vehicle Concept
AIAA-2005-4190, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
July 10-13, 2005, Tucson, AZ.

Rohrschneider, R.R., and Braun, R.D.
A Survey of Ballute Technology for Aerocapture
Proceedings of the 3rd International Planetary Probe Workshop
June 2005, Athens, Greece.

Kipp, D.M.; Dec, J.A.; Wells, G.M.; and Braun, R.D.
Development of a Planetary Entry System Synthesis Tool for Conceptual Design and Analysis
Proceedings of the 3rd International Planetary Probe Workshop
June 2005, Athens, Greece.

Young, D., Olds, J.
Responsive Access Small Cargo Affordable Launch (RASCAL) Independent Performance Evaluation
AIAA 2005-3241, 13th International Space Planes and Hypersonics Systems and Technologies Conference
May 2005, Capua, Italy

Clark, I., Francis, S., Otero, R., Wells, G.
Reusable Exploration Vehicle (REV): Orbital Space Tourism Concept
2005 RASC-AL Design Competition
May 2005, Coco Beach, FL.

Thompson, R.W., Francis, S.R., Olsen, R,. Parsons, M., Coffman, R., and Braun, R.D.
Cadmus: A Europa Lander Mission Concept
IEEE 05-1577, IEEE Aerospace Conference
March 2005, Big Sky MT,

Christian, J., Olds, J.
A Quantitative Methodology for Identifying Evolvable Space Systems
AIAA 2005-2543, 1st AIAA Space Exploration Conference
January 2005, Orlando, FL.

LaFleur, J.M., Olds, J., and Braun, R.D.
Daedalon: A Revolutionary Morphing Spacecraft Design for Planetary Exploration
AIAA 05-2771, 1st AIAA Space Exploration Conference
January 2005, Orlando FL.

Sakai, T., Olds, J., Alemany, K.
Development of SAMURAI - Simulation and Animation Model Used for Rockets with Adjustable Isp.
AAS 05-181, 15th AAS/AIAA Space Flight Mechanics Conference
January 2005, Copper Mountain, CO.

Rohrschneider, R.R., Olds, J.R., Kuhl, C.A., Braun, R.D., Steffes,
S.R., and Hutchinson V.
Flight System Options for a Long Duration Mars Airplane
AIAA 2004-6568, 3rd AIAA "Unmanned Unlimited" Technical Conference
Chicago, IL, Sept. 20-23, 2004.

Hutchinson Jr., V. and Olds, J.R.
Estimation of Launch Vehicle Propellant Tank Structural Weight Using Simplified Beam Approximation
AIAA 2004-3661, 40th IAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Fort Lauderdale, FL, July 11-14, 2004.

Young, D., Olds, J.R., Hutchinson, V., Krevor, Z., Pimentel, J., Reeves, J.D., Sakai, T., Young, J.
Centurion: A Heavy-Lift Launch Vehicle Family for Cis-Lunar Exploration
AIAA 2004-3735, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference And Exhibit
Fort Lauderdale, FL, July 11 - 14, 2004.

Biltgen, P., Lafleur, J., Loughman, J., Martin, R., Flaherty, K., Cho, M., Becker, K., Ong, C., Olds, J.R.
StarRunner: A Single-Stage-to-Orbit, Airbreathing, Hypersonic Propulsion System
AIAA 2004-3729, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference And Exhibit
Fort Lauderdale, FL, July 11-14, 2004.

Kokan, T., Hutchinson, V., Reeves, J.D., Olds, J.R.
Aztec: A TSTO Hypersonic Vehicle Concept Utilizing TBCC and HEDM Propulsion Technologies
AIAA 2004-3728, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference And Exhibit
Fort Lauderdale, FL, July 11 - 14, 2004.

Rohrschneider, R., Olds, J.R., Braun, R., Hutchinson, V., Kuhl, C., Steffes, S.
Modeling Approach for Analysis and Optimization of a Long-Duration Mars Airplane
AIAA 2004-4313, AIAA MA&O Conference
Albany, NY, May 30-June 1, 2004.

Young, J., Alemany, K., Cole, B., Depasquale, D., Dvilyanski, M., Fornuff, J.
A Multi-Role Architecture Using Turbine Based Combined Cycle
2004 RASC-Al Design Competition
Fort Lauderdale, FL, July 11 - 14, 2004.

Braun, R.D.; Wright, H.S.; Croom, M.A.; Levine, J.S.; and Spencer, D.A.
The Mars Airplane: A Credible Science Platform
IEEE 04-1260, IEEE Aerospace Conference
Big Sky MT, March 2004.

Sakai, T., Olds, J.R.
Development of a Multipurpose Low Thrust Interplanetary Trajectory Calculation Code
AAS03-667, AAS/AIAA Astrodynamics Specialist Conference
Big Sky, MT, August 3 - 7, 2003.

Steffes, S. R., Olds, J. R.
Magel: An Advanced Partially Reusable Launch Architecture Concept
AIAA-2003-7054, 12th AIAA International Space Planes and Hypersonic Systems and Technologies
Norfolk, VA, December 15-19, 2003.

Crowley, J., Hutchinson, V., Keisner, A., Young, D., Curry, M., Jackson, J., Maatsch J., Piletsky, P., Olds, J.
Chimera: A Low Cost Solution to Small Satellite Space Access
SSC03-VII-2, In the Proceedings of the 17th Annual AIAA/USU Conference on Small Satellites, UT State University
Logan, UT, August 11 -14, 2003.

St. Germain, B., Kokan, T., Marcus, L., Miller, J., Rohrschneider, R., Staton, E., Olds, J.
Tanker Argus: Re-supply for a LEO Cryogenic Propellant Depot
IAC-02-V.P.10, 53rd International Astronautical Congress, The World Space Congress
Houston, TX, October 10-19, 2002.

Rohrschneider, R., Sakai, T., Steffes, S., Grillmayer, G., St. Germain, B., Olds, J.
Solar Electric Propulsion Module Concept for the BiFrost Architecture
IAC-02-S.4.09, 53rd International Astronautical Congress, The World Space Congress
Houston, TX, October 10-19, 2002.

McCormick, D., Olds, J.
A Distributed Framework for Probabilistic Analysis
AIAA 2002-5587, 2002 AIAA/ISSMO Symposium on Multidisciplinary Analysis and Design Optimization
Atlanta, GA, September 4-6, 2002.

McCormick, D., Olds, J.
A Design of Experiments-Based Method for Point Selection in Approximating Output Distributions
AIAA 2002-5535, 2002 AIAA/ISSMO Symposium on Multidisciplinary Analysis and Design Optimization
Atlanta, GA, September 4-6, 2002.

Kokan, T., Olds, J.
Mission Capture Rate versus Turnaround Time and Fleet Size for the Military Spaceplane
AIAA 2002-3905, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference And Exhibit
Indianapolis, IN, July 7-10, 2002.

Marcus, L., Way, D., Medlin, M., Sakai, T., McIntire, J., Olds, J.
Technology Assessment for Manned Mars Exploration Using a ROSETTA Model of a Bimodal Nuclear Thermal Rocket (BNTR)
AIAA 2001-4623, AIAA Space 2001 Conference and Exposition, Albuquerque, New Mexico, August 28-30, 2001.

Rohrschneider, R., Olds, J.
A Comparison of Modern and Historic Mass Estimating Relationships on a Two-Stage to Orbit Launch Vehicle
AIAA 2001-4542, AIAA Space 2001 Conference and Exposition
Albuquerque, New Mexico, August 28-30, 2001.

Nelson, D., Marcus, L., Bechtel, R., Cormier, T., Weglian, J., Alexander, R.
Moon-based Advanced Reusable Transportation Architecture
AIAA 2001-3524, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference And Exhibit
Salt Lake City, UT, July 8-11, 2001.

St. Germain, B., Olds, J., McIntire, J., Nelson, D., Weglian, J., Ledsinger, L.
Starsaber: A Small Payload-Class TSTO Vehicle Concept Utilizing Rocket-Based Combined Cycle Propulsion
AIAA 2001-3516, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference And Exhibit
Salt Lake City, UT, July 8-11, 2001.

Weglian, J., Olds, J., Marcus, L., McIntire, J., Nelson, D., Blevins, J.
ASPEN Revisited: The Challenge of Nuclear Propulsion for ETO
AIAA-2001-3514, 37th AIAA/ ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Salt Lake City, UT, July 8-11, 2001.

Charania, A., Olds, J.
A Unified Economic View of Space Solar Power (SSP)
IAA-00-R.1.06, 51st International Astronautical Congress
Rio de Janeiro, Brazil, October 2-6, 2000.

Olds, J., Way, D., Charania, A., Budianto, I., Marcus, L.
In-Space Deployment Options for Large Space Solar Power Satellites
IAA-00-R.2.02, 51st International Astronautical Congress
Rio de Janeiro, Brazil, October 2-6, 2000.

Olds, J., McCormick, D., Charania, A., Marcus, L.
Space Tourism: Making it Work for Fun and Profit
IAA-00-IAA.1.3.05, 51st International Astronautical Congress
Rio de Janeiro, Brazil, October 2-6, 2000.

Cowart, K., Olds, J.
TCAT - A Tool For Automated Thermal Protection System Design
AIAA 2000-5265, AIAA Space 2000 Conference and Exposition
Long Beach, CA, September 19-21, 2000.

Bradford, J., Olds, J., Bechtel, R., Cormier, T., Messitt, D.
Exploration of the Design Space for the ABLV-GT SSTO Reusable Launch Vehicle
AIAA 2000-5136, AIAA Space 2000 Conference and Exposition
Long Beach, CA, September 19-21, 2000.

Cormier, T., Scott, A., Ledsinger, L., McCormick, D., Way, D., Olds, J.
Comparison of Collaborative Optimization to Conventional Design Techniques for a Conceptual RLV
AIAA 2000-4885, 8th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
Long Beach, CA, September 6-8, 2000.

Ledsinger, L., Olds, J.
Optimized Solutions for the Kistler K- 1 Branching Trajectory Using MDO Techniques
AIAA 2000-4884, 8th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
Long Beach, CA, September 6-8, 2000.

McCormick, D., Olds, J.
Approximation of Probabilistic Distributions Using Selected Discrete Simulations
AIAA 2000-4863, 8th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
Long Beach, CA, September 6-8, 2000.

Budianto, I., Olds, J.
A Collaborative Optimization Approach to Design and Deployment of a Space Based Infrared System Constellation
IEEE P335E, 2000 IEEE Aerospace Conference
Big Sky, MT, March 18-25, 2000.

Olds, J., Bradford, J., Charania, A., Ledsinger, L., McCormick, D., Sorensen, K.
Hyperion: An SSTO Vision Vehicle Concept Utilizing Rocket-Based Combined Cycle Propulsion
AIAA 99-4944, 9th International Space Planes and Hypersonic Systems and Technologies Conference
Norfolk, VA, November 1-5, 1999.

Olds, J., Ledsinger, L., Bradford, J., Charania, A., McCormick, D., Komar, D. R.
Stargazer: A TSTO Bantam-X Vehicle Concept Utilizing Rocket-Based Combined Cycle Propulsion
AIAA 99-4888, 9th International Space Planes and Hypersonic Systems and Technologies Conference
Norfolk, VA, November 1-5, 1999.

Cowart, K., Olds, J.
Integrating Aeroheating and TPS into Conceptual RLV Design
AIAA 99-4806, 9th International Space Planes and Hypersonic Systems and Technologies Conference
Norfolk, VA, November 1-5, 1999.

St. Germain, B. D., Olds, J. R.
An Evaluation of Two Alternate Propulsion Concepts for Bantam-Argus: Deeply-Cooled Turbojet+Rocket and Pulsed Detonation Rocket+Ramjet
AIAA 99-2354, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Los Angeles, CA, June 20-24, 1999.

Way, D. W., Olds, J. R.
SCORES: Web-Based Rocket Propulsion Analysis Tool for Space Transportation System Design
AIAA 99-2353, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Los Angeles, CA, June 20-24, 1999.

Bradford, J. E., Olds, J. R.
SCCREAM v.5: A Web-Based Airbreathing Propulsion Analysis Tool
AIAA 99-2104, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Los Angeles, CA, June 20-24, 1999.

Budianto, I. A., Olds, J. R. and Baker, N. C.
Demonstration of CLIPS as an Intelligent Front-End for POST
AIAA 99-0110, 37th Aerospace Sciences Meeting and Exhibit
Reno, NV, January 11-14, 1999.

McCormick, D. J., and Olds, J. R.
System Robustness Comparison of Advanced Space Launch Concepts
AIAA 98-5209, 1998 Defense and Civil Space Programs Conference and Exhibit
Huntsville, AL, October 28-30, 1998.

Scott, J. M. and Olds, J. R.
Transforming Aerodynamic Datasets into Parametric Equations for use in Multi-disciplinary Design Optimization
AIAA 98-5208, 1998 Defense and Civil Space Programs Conference and Exhibit
Huntsville, AL, October 28-30, 1998.

Whitfield, J. A. and Olds, J. R.
Economic Uncertainty of Weight and Market Parameters for Advanced Space Launch Vehicles
AIAA 98-5179, 1998 Defense and Civil Space Programs Conference and Exhibit
Huntsville, AL, October 28-30, 1998.

Acton, D. E. and Olds, J. R.
Computational Frameworks for Collaborative Multidisciplinary Design of Complex Systems
AIAA 98-4942, 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
St. Louis, MO, September 2-4, 1998.

Olds, J. R. and Steadman, K. B.
Cross-Platform Computational Techniques for Analysis Code Integration and Optimization
AIAA 98-4743, 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
St. Louis, MO, September 2-4, 1998.

Ledsinger, L. A. and Olds, J. R.
Multidisciplinary Design Optimization Techniques for Branching Trajectories
AIAA 98-4713, 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
St. Louis, MO, September 2-4, 1998.

Bradford, J. E. and Olds, J. R.
Improvements and Enhancements to SCCREAM, A Conceptual RBCC Engine Analysis Tool
AIAA 98-3775, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Cleveland, OH, July 12 - 15, 1998.

Way, D. W. and Olds, J. R.
SCORES: Developing an Object-Oriented Rocket Propulsion Analysis Tool
AIAA 98-3227, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Cleveland, OH, July 12 - 15, 1998.

Olds, J. R. and Bellini, P. X.
Argus, a Highly Reusable SSTO Rocket-Based Combined Cycle Launch Vehicle with Maglifter Launch Assist
AIAA 98-1557, AIAA 8th International Space Planes and Hypersonic Systems and Technologies Conference
Norfolk, VA, April 1998.

Olds, J. R. and Ledsinger, L. A.
Multidisciplinary Optimization Techniques for Branching Trajectories
A companion paper to an AIAA Off-the-Drawing-Board Presentation, 36th Aerospace Sciences Meeting and Exhibit
Reno, NV, January 1998.

Olds, J. R. and Budianto, I. A.
Constant Dynamic Pressure Trajectory Simulation in POST
AIAA 98-0302, 36th Aerospace Sciences Meeting and Exhibit
Reno, NV, January 1998.

Olds, J. R. and McCormick, D. J.
Component-Level Weight Analysis for RBCC Engines
AIAA 97-3953, 1997 Defense and Space Programs Conference and Exhibit
Huntsville, AL, September 1997.

Lee, H. and Olds, J. R.
Integration of Cost and Business Simulation into Conceptual Launch Vehicle Design
AIAA 97-3911, 1997 Defense and Space Programs Conference and Exhibit
Huntsville, AL, September 1997.

Way, D.W. and Olds, J. R.
Sirius: A New Launch Vehicle Option for Mega-LEO Constellation Deployment
AIAA 97-3122, 33rd AIAA/ASME/ SAE/ASEE Joint Propulsion Conference and Exhibit
Seattle, WA, July 1997.

Olds, J. R. and Bradford, J. E.
SCCREAM (Simulated Combined-Cycle Rocket Engine Analysis Module): A Conceptual RBCC Engine Design Tool
AIAA 97-2760, 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Seattle, WA, July 1997.

Olds, J. R. and Saks, G.
A Conceptual Design Tool for RBCC Engine Performance Analysis
Proceedings of the 1997 Space Technology & Applications International Forum
American Institute of Physics and the University of New Mexico
Albuquerque, NM, January 1997.

Olds, J. R. and Lee, H.
Application of a New Economic Analysis Tool to a Two-Stage-to-Orbit RBCC Launch Vehicle Design
AIAA 96-4092, 6th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization,
Bellevue, WA, September 1996.

Olds, J. R.
Options for Flight Testing Rocket-Based Combined-Cycle (RBCC) Engines
AIAA 96-2688, 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Lake Buena Vista, FL, July 1996.

Olds, J.R.
System Sensitivity Analysis Applied to the Conceptual Design of a Dual-Fuel Rocket SSTO
AIAA 94-4339, 5th AIAA/USAF/NASA/ISSMO  Symposium on Multidisciplinary Analysis and Optimization,                                                                                                  Panama City, Fl, September 1994.

Olds, J.R.
Results of a Rocket-Based Combined-Cycle SSTO Design Using Parametric  MDO Methods
SAE 94-1165, 1994 Aerospace Atlantic Conference,                                                  Dayton, OH, April 1994.

Olds, J.R. and Walberg, G.
Multidisciplinary Design of a RBCC SSTO using Taguchi Methods
AIAA 93-1096, AIAA/AHS/ASEE Aerospace Design Conference,                                 Irvine, CA, February 1993.

Olds, J.R.
The Suitability of Selected Multidisciplinary Design and Optimization Techniques to Conceptual Aerospace Vehicle Design
AIAA 92-4791, 4th AIAA/USA/NASA/OAI Symposium on Multidisciplinary Analysis and Optimization,                                                                                                         Cleveland, OH, September 1992.

Olds, J.R.
A Conceptual Design for a SSTO Space Station Service Vehicle
IAF ST-87-07, 38th Congress of the International Astronautical Federation,                  Brighton, UK, October 1987.