Entry, Descent and Landing Systems Analysis Study: Phase 2 Report on Exploration Feed-Forward Systems
Alicia M. Dwyer Ciancolo, Jody L. Davis, Walter C. Engelund, David R. Komar, Eric M. Queen, Jamshid A. Samareh, David W. Way, Thomas A. Zang, Jeff G. Murch, Shawn A. Krizan, Aaron D. Olds, Richard W. Powell, Jeremy Shidner, Daivd J. Kinney, Mary K. McGuire, James O. Arnold, M. A. Covington, Ronald R. Sostaric, Carlie H. Zumwalt, Eduardo Garcia Llama
- 发表年份
- 2011
- 引用次数
- 27
摘要
NASA senior management commissioned the Entry, Descent and Landing Systems Analysis (EDL-SA) Study in 2008 to identify and roadmap the Entry, Descent and Landing (EDL) technology investments that the agency needed to successfully land large payloads at Mars for both robotic and human-scale missions. Year 1 of the study focused on technologies required for Exploration-class missions to land payloads of 10 to 50 t. Inflatable decelerators, rigid aeroshell and supersonic retro-propulsion emerged as the top candidate technologies. In Year 2 of the study, low TRL technologies identified in Year 1, inflatables aeroshells and supersonic retropropulsion, were combined to create a demonstration precursor robotic mission. This part of the EDL-SA Year 2 effort, called Exploration Feed Forward (EFF), took much of the systems analysis simulation and component model development from Year 1 to the next level of detail.
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