His primary areas of investigation include Aerospace engineering, Mars Exploration Program, Aerodynamics, Atmosphere of Mars and Descent. His work on Aerocapture and Aerobraking as part of his general Aerospace engineering study is frequently connected to Sizing, thereby bridging the divide between different branches of science. His Mars Exploration Program research integrates issues from Atmospheric entry, Aeronautics, Space Shuttle thermal protection system and Propellant mass fraction.
In general Aerodynamics, his work in Aeroshell is often linked to Environmental science linking many areas of study. His study in Atmosphere of Mars is interdisciplinary in nature, drawing from both Pitching moment, Angle of attack, Dynamic pressure and Geodesy. In his research on the topic of Descent, Operations research and Simulation is strongly related with Payload.
Robert D. Braun mainly focuses on Aerospace engineering, Mars Exploration Program, Aerodynamics, Trajectory and Exploration of Mars. His work on Supersonic speed, Aerocapture, Descent and Hypersonic speed is typically connected to Environmental science as part of general Aerospace engineering study, connecting several disciplines of science. His Descent research includes themes of Aeronautics and Mars entry.
His work deals with themes such as Atmospheric entry and Spacecraft, which intersect with Mars Exploration Program. His Aerodynamics research is multidisciplinary, incorporating perspectives in Drag, Structural engineering, Inflatable and Conceptual design. He interconnects Crew, Ballistic coefficient, Payload and Range in the investigation of issues within Exploration of Mars.
His scientific interests lie mostly in Aerospace engineering, Aerocapture, Mars Exploration Program, Environmental science and Space Shuttle thermal protection system. His study ties his expertise on Aeronautics together with the subject of Aerospace engineering. His Aerocapture study also includes fields such as
His Exploration of Mars, In situ resource utilization and Atmosphere of Mars study, which is part of a larger body of work in Mars Exploration Program, is frequently linked to Molniya orbit, bridging the gap between disciplines. His Space Shuttle thermal protection system research includes elements of Hypersonic speed and Conformal map. His Descent study integrates concerns from other disciplines, such as Gravity turn and Thrust.
His primary scientific interests are in Aerospace engineering, Mars Exploration Program, Supersonic speed, Environmental science and Space Shuttle thermal protection system. His work carried out in the field of Aerospace engineering brings together such families of science as Aeronautics and Orbit. Robert D. Braun has included themes like Ballistic coefficient and Trajectory in his Mars Exploration Program study.
His Ballistic coefficient research incorporates elements of Orbit of Mars, Mars landing and Crew. His Space Shuttle thermal protection system research incorporates themes from Optoelectronics, Conformal map and Nanotechnology. He combines subjects such as Hypersonic speed, Mars entry, Aerodynamics and Inflatable with his study of Descent.
This overview was generated by a machine learning system which analysed the scientist’s body of work. If you have any feedback, you can contact us here.
Mars Exploration Entry, Descent, and Landing Challenges
Robert D. Braun;Robert M. Manning.
Journal of Spacecraft and Rockets (2007)
Collaborative optimization: an architecture for large-scale distributed design
Robert David Braun.
(1996)
Development and Application of the Collaborative Optimization Architecture in a Multidisciplinary Design Environment
R D Braun;I M Kroo.
(1995)
Implementation and Performance Issues in Collaborative Optimization
R D Braun;P J Gage;I M Kroo;I Sobiesiki.
6th Symposium on Multidisciplinary Analysis and Optimization (1996)
Use of the Collaborative Optimization Architecture for Launch Vehicle Design
R D Braun;A A Moore;I M Kroo.
6th Symposium on Multidisciplinary Analysis and Optimization (1996)
Collaborative Approach to Launch Vehicle Design
R. D. Braun;A. A. Moore;I. M. Kroo.
Journal of Spacecraft and Rockets (1997)
Mars Pathfinder Entry, Descent, and Landing Reconstruction
David A. Spencer;Robert C. Blanchard;Robert D. Braun;Pieter H. Kallemeyn.
Journal of Spacecraft and Rockets (1999)
Technology Readiness Level, Schedule Risk, and Slippage in Spacecraft Design
Gregory F. Dubos;Joseph H. Saleh;Robert Braun.
Journal of Spacecraft and Rockets (2008)
Influence of sonic-line location on Mars Pathfinder Probe aerothermodynamics
Peter A. Gnoffo;K. J. Weilmuenster;Robert D. Braun;Christopher I. Cruz.
Journal of Spacecraft and Rockets (1996)
Guidance, Navigation, and Control System Performance Trades for Mars Pinpoint Landing
Bradley A. Steinfeldt;Michael J. Grant;Daniel A. Matz;Robert D. Braun.
Journal of Spacecraft and Rockets (2010)
If you think any of the details on this page are incorrect, let us know.
We appreciate your kind effort to assist us to improve this page, it would be helpful providing us with as much detail as possible in the text box below:
Stanford University
Langley Research Center
Langley Research Center
Ames Research Center
Ames Research Center
Courant Institute of Mathematical Sciences
Hong Kong University of Science and Technology
Hunan University
General Electric (United States)
Lund University
Osaka University
Vrije Universiteit Amsterdam
MSD (United States)
American Museum of Natural History
Northwestern University
Cornell University
Sorbonne University
University of Western Australia
University of Cincinnati
University of Connecticut Health Center
Hebrew University of Jerusalem