| Experimental investigation of a Mach 3.5 waverider designed using computational fluid dynamics MA Lobbia, K Suzuki AIAA Journal 53 (6), 1590-1601, 2015 | 56 | 2015 |
| Multidisciplinary design optimization of waverider-derived crew reentry vehicles MA Lobbia Journal of Spacecraft and Rockets 54 (1), 233-245, 2017 | 41 | 2017 |
| Multidisciplinary design optimization of hypersonic transport configurations using waveriders M Lobbia, K Suzuki 19th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2014 | 32 | 2014 |
| Design and analysis of payload-optimized waveriders M Lobbia, K Suzuki 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems …, 2001 | 27 | 2001 |
| Rapid supersonic/hypersonic aerodynamics analysis model for arbitrary geometries MA Lobbia Journal of Spacecraft and Rockets 54 (1), 315-322, 2017 | 24 | 2017 |
| A modular sizing model for high-altitude/long-endurance airships M Lobbia, R Gong 44th AIAA aerospace sciences meeting and exhibit, 821, 2006 | 22 | 2006 |
| Numerical investigation of waverider-derived hypersonic transport configurations M Lobbia, K Suzuki 21st AIAA applied aerodynamics conference, 3804, 2003 | 20 | 2003 |
| Affordability assessments to support strategic planning and decisions at NASA DL Emmons, M Lobbia, T Radcliffe, RE Bitten 2010 IEEE Aerospace Conference, 1-13, 2010 | 17 | 2010 |
| Optimization of waverider-derived crew reentry vehicles using a rapid aerodynamics analysis approach M Lobbia 53rd AIAA Aerospace Sciences Meeting, 0757, 2015 | 16 | 2015 |
| Validation of a high-fidelity supersonic parachute inflation dynamics model and best practice F As' ad, P Avery, C Farhat, J Rabinovitch, M Lobbia AIAA SCITECH 2022 Forum, 0351, 2022 | 13 | 2022 |
| An analogy-based method for estimating the costs of spacecraft R Kellogg, E Mahr, M Lobbia 2005 IEEE Aerospace Conference, 4441-4447, 2005 | 13 | 2005 |
| Hybrid propulsion Mars Ascent Vehicle concept flight performance analysis J Benito, C Noyes, R Shotwell, A Karp, B Nakazono, G Singh, H Kim, ... 2017 IEEE Aerospace Conference, 1-13, 2017 | 12 | 2017 |
| The evolution of an orbiting sample container for potential Mars sample return S Perino, D Cooper, D Rosing, L Giersch, Z Ousnamer, V Jamnejad, ... 2017 IEEE Aerospace Conference, 1-16, 2017 | 11 | 2017 |
| A framework for the design and optimization of waverider-derived hypersonic transport configurations M Lobbia University of Tokyo, Tokyo, 2004 | 11 | 2004 |
| ASPIRE2: The Mars Sample Retrieval Lander's Supersonic Parachute Test Program C O'Farrell, EA Leylek, MA Lobbia, KJY Siegel 2023 IEEE Aerospace Conference, 1-9, 2023 | 8 | 2023 |
| Update: Modeling Supersonic Parachute Inflations for Mars Spacecraft J Rabinovitch, F As’ ad, P Avery, C Farhat, N Ataei, M Lobbia 26th AIAA Aerodynamic Decelerator Systems Technology Conference, 2746, 2022 | 8 | 2022 |
| InSight EDL Overview and As-Flown Performance C Zumwalt, E Sklyanskiy, M Lobbia, E Leylek, S Francis, E Bonfiglio, ... Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space …, 2019 | 4 | 2019 |
| Design of waveriders from conical and blunt-body flowfields M Lobbia, K Suzuki International Symposium on Space Technology and Science, 22 nd, Morioka …, 2000 | 3 | 2000 |
| Mars Ascent Vehicle concept-overview and aeroheating/thermal protection system design R Shotwell, J Benito, A Korzun, M Lobbia Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space …, 2017 | 2 | 2017 |
| 1-D Heat Transfer in Multilayer Materials Using a Finite Volume Approach MA Lobbia, AFS Command The Aerospace Corporation, 2014 | 2 | 2014 |
