Mars entry, descent, and landing parametric sizing and design space visualization trades

Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006

Volumn 1, Issue , 2006, Pages 122-133

  Alemany, Kristina ^a,b   Wells, Grant ^a,b   Theisinger, John ^a,b   Claik, Ian ^a,b   Braun, Robert ^a,b  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DECISION MAKING; MARTIAN SURFACE ANALYSIS; PARAMETER ESTIMATION; PLANETARY LANDERS; REENTRY; SPACE APPLICATIONS;

MARS ENTRY; SPACE EXPLORATION; SPACE VISUALIZATION; SYSTEMATIC VISUALIZATION;

SPACE FLIGHT;

EID: 33846005779     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-6022     Document Type: Conference Paper

References (4)

1. th International Planetary Probe Workshop, June 2005, Athens, Greece.
2. rd International Planetary Probe Workshop, June 2005, Athens, Greece.
3. Dec., John A., Braun, R.D., "An Approximate Ablative Thermal Protection System Sizing Tool for Entry System Design," AIAA Aerospace Sciences Meeting and Exhibit, January 2006, Reno, NV.
4. Braun, R.D., Manning, R.M., "Challenges of Mars Entry, Descent, and Landing," IEEE Aerospace Conference, March 2006, Big Sky, MT.