- Transportation and Resources in the CisLunar Marketplace (CIM Convention, May 2017)
- CisLunar Marketplace Workshop (Space Symposium, April 2017)
- CisLunar Marketplace Workshop (February 2017)
- CisLunar-1000: Transportation Supporting a Self-Sustaining Space Economy (AIAA Space 2016)
- Transportation Enabling a Robust Cislunar Space Economy (Space Resources Roundtable, Planetary & Terrestrial Mining Sciences Symposium June 2016)
- Transportation Enabling a Robust Cislunar Space Economy (Space Access and Northeastern Astronomy Forum April 2016)
- Transportation Architecture for Cislunar Space (Space Solar Power 2015)
- The Business Case for Space (AIAA Space 2015)
- AIAA Paper on NRO Space 2012
- Commercial Launch Services: An Enabler for Launch Vehicle Evolution and Cost Reduction 2006-7271
- Response to NASA RFI for Commercial Space Transportation
- AIAA paper on DSS 4 and DSS 5 2011-09-12
- Innovation at ULA (AIAA Space 2016)
- Vulcan, ACES and Beyond: Providing Launch Services for Tomorrow's Spacecraft (American Astronomical Society 2016)
- Upper Stage Extensibility for Testbed Applications
- GPS Metric Tracking
- RD-180 Engine: An Established Record of Performance and Reliability on Atlas Launch Vehicles
- Single Event Upset Testing of Commercial Off-The-Shelf Electronics for Launch Vehicle Applications
- United Launch Alliance - Establishing Heavy Lift Capability on the West Coast
- EELV Partially Reusable Booster 2010
- EELV Phase 2 – An Old Configuration Option with New Relevance to Future Heavy Lift Cargo
- Atlas I to Atlas V: The Path to an Affordable and Operationally Efficient Launch System 2006-5927
- Booster Innovation Presentation 2009
- Critical Events of the Inaugural Launch of the Boeing Delta IV Expendable Launch Vehicle
- Delta IV Launch Vehicle Growth Options to Support NASA's Space Exploration Vision
- Dual Spacecraft System 2008-7658
- Dual Spacecraft System 2009
- Evolved Atlas To Meet Space Transportation Needs 2005-6815
- Partial Rocket Reuse Using Mid-Air Recovery 2008-7874
- The Next-Generation Heavy-Lift Vehicle — The Inaugural Flight of the EELV Delta IV Heavy
- What Makes An Affordable and Reliable Launch System 2006-7210
- Cryogenic Propulsive Stage Mission Sensitivity Studies - Earth-Moon L1 Departure
- Cryogenic Propulsive Stage Mission Sensitivity Studies: Low Earth Orbit Departure
- Evolving to a Depot-Based Space Transportation Architecture
- Lunar Lander Configurations Incorporating Accessibility 2006-7284
- Affordable Exploration Architecture 2009
- Dual Thrust Axis Lander (DTAL) 2009
- Atlas V LRO LCROSS Mission Overview 2011
- Enabling Long Duration Spaceflight via an Integrated Vehicle Fluid System (AIAA Space 2016)
- Distributed Launch - Enabling Beyond LEO Missions (AIAA Space 2015)
- Development Status of an Integrated Propulsion and Power System for Long Duration Cryogenic Spaceflight 2012
- Cryogenic Orbital Test Bed Development
- Micro-gravity Cryogenic Experiment Opportunity
- A Practical, Affordable Cryogenic Propellant Depot Based on ULA's Flight Experience
- Atlas Centaur Extensibility to Long-Duration In-Space Applications
- Centaur Extensibility for Long Duration 2006-7270
- Design and Development of an In-space Deployable Sun Shield for the Atlas Centaur
- Settled Cryogenic Propellant Transfer 2006-4436
- Cryogenic Orbital Testbed (CRYOTE) 2009
- Propellant Depots 2009
- Propellant Depot JPC Presentation 2009
- Atlas Centaur Sun Shield Design and Testing: An Update 2009
- Integrated Vehicle Propulsion and Power System 2011
- CRYOTE Cryo Workshop 2011
- Commercial Crew Abort System Design Evolution and Validation (AIAA Space 2015)
- Commercial Crew Launch Emergency Detection System: The Key Technology for Human Rating EELV
- Enabling Crew Launch on Atlas V and Delta IV
- Atlas Emergency Detection System
- Atlas V: Safe and Affordable Human Spaceflight 2005-6706
- Atlas V for Commercial Passenger Transportation 2006-7268
- ELV Human Rating: Atlas Heritage and Future Potential 2005-3812
- EELV Considerations - Briefing to the Review of U.S. Human Space Flight Plans Committee
- Human Rating Atlas V and Delta IV
- Advantages of Heritage Atlas Systems for Human Spaceflight 2011
- Evolution of Abort Management of Crewed Launch Vehicles 2011
- Commercial Crew Development Enabling Launch on EELV 2011
- CubeSat Express: The Future of Rideshare Launch (CubeSat Developer's Workshop, May 2017)
- ULA Rideshare Overview (2015)
- The Atlas V Aft Bulkhead Carrier Update - Past Missions, Upcoming Launches and Future Improvements (AIAA/USU Small Sat 2015)
- ULA SmallSat/Hosted Rideshare Mission Accommodations (AIAA Space 2013)
- ULA Rideshare Capabilities for Providing Low-cost Access to Space
- ULA Rideshare Capabilities to Support Low-Cost Planetary Missions (2011)
- The Atlas V Aft Bulkhead Carrier - Requirements for the Small Satellite Designer (AIAA/USU Small Sat 2010)
- Small Satellite Access to ESPA Standard Service (AIAA/USU Small Sat 2010)
- EELV Secondary Payloads Accommodations (2007)
- Launch Vehicle Recovery and Reuse (AIAA Space 2015)
- Additive Manufacturing Efforts and Applications in Expendable Launch Vehicles
- Orbital Disposal of Launch Vehicle Upper Stages
- Space Access Society 2012
- Error Prevention Process Overview
- ULA Error Prevention Program – Learning From Mistakes
- Ordnance Safety Requirements for Space Launch Vehicles
- Delta Qualification Test of Aerojet Hydrazine Thrusters for Use on Centaur during the LRO and LCROSS Missions 2009-5481
- Innovative Technologies for Improved Launch Probability — Delta IV Day-of-Launch Monitoring
- Successful Flight Demonstration Conducted by the Air Force and United Launch Alliance Will Enhance Space Transportation
- ULA Delta IV Vehicle—An Update to the Pulse Settling Propellant Management Approach
- Ongoing Launch Vehicle Innovation at United Launch Alliance
- Incorporation of RD-180 Failure Response 2011
- XEUS: A Powerful Path to Beyond LEO Activity (Space Symposium 2017)
- ACES Stage Concept: Higher Performance, New Capabilities, at a Lower Recurring Cost (AIAA Space 2015)
- Centaur Upperstage Applicability for Several-Day Mission Durations with Minor Insulation Modifications 2007-5845
- Centaur Application to Robotic and Crewed Lunar Lander Evolution
- Centaur Test Bed (CTB) for Cryogenic Fluid Management 2006-4603
- History of the Titan Centaur Launch Vehicle
- Upper Stage Evolution Presentation 2009
- GH2 Orbital Space Transfer (GHOST) 2009
- The Advanced Cryogenic Evolved Stage (ACES) — A Low-Cost, Low-Risk Approach to Space Exploration Launch
- The Centaur Upper Stage Vehicle