Add to ORKGDevelop two evolutionary rigid vehicle concepts to deliver human-scale payloads (20 metric tons) to the surface of Mars: Capsule; Lifting body, mid-range lift-to-drag ratio (Mid L/D). Determine vehicle configurations for various mission flight phases. Determine vehicle performance: Integrated system mass; Ability to meet landing constraints; Payload packaging and surface access. Provide technology investment recommendations to NASAs Space Technology Mission Directorate
29th AAS Guidance and Control Conference February 2006, Breckenridge, CO.Near-term capabilities for...
As the agency space transportation lead center, Marshall Space Flight Center has been conducting tra...
IEEE Aerospace Conference March 2006, Big Sky, MT.The United States has successfully landed five r...
Several technology investments are required to develop Mars human scale Entry, Descent, and Landing ...
NASAs Entry, Descent and Landing Architecture Study uses a trajectory simulation framework to evalua...
Current NASA Human Mars architectures require delivery of approximately 20 metric tons of cargo to t...
This paper explores the impact of human Mars mission architecture decisions on the design and perfor...
In an effort to mature the design of the Mid-Lift-to-Drag ratio Rigid Vehicle (MRV) candidate of the...
AIAA Space 2006 Conference September 2006, San Jose, CA.The human exploration of Mars presents many...
Landing humans on Mars is one of NASA's long term goals. NASA's Evolvable Mars Campaign (EMC) is foc...
Entry mass at Mars is limited by the payload size that can be carried by a rigid capsule that can fi...
Human-scale landers require the delivery of much heavier payloads to the surface of Mars than is pos...
The Mid-Lift-to-Drag Ratio Rigid Vehicle (MRV) is a proposed candidate in the NASA Evolvable Mars Ca...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.Th...
Defining a feasible vehicle design and mission architecture capable of reliably delivering apayload ...
29th AAS Guidance and Control Conference February 2006, Breckenridge, CO.Near-term capabilities for...
As the agency space transportation lead center, Marshall Space Flight Center has been conducting tra...
IEEE Aerospace Conference March 2006, Big Sky, MT.The United States has successfully landed five r...
Several technology investments are required to develop Mars human scale Entry, Descent, and Landing ...
NASAs Entry, Descent and Landing Architecture Study uses a trajectory simulation framework to evalua...
Current NASA Human Mars architectures require delivery of approximately 20 metric tons of cargo to t...
This paper explores the impact of human Mars mission architecture decisions on the design and perfor...
In an effort to mature the design of the Mid-Lift-to-Drag ratio Rigid Vehicle (MRV) candidate of the...
AIAA Space 2006 Conference September 2006, San Jose, CA.The human exploration of Mars presents many...
Landing humans on Mars is one of NASA's long term goals. NASA's Evolvable Mars Campaign (EMC) is foc...
Entry mass at Mars is limited by the payload size that can be carried by a rigid capsule that can fi...
Human-scale landers require the delivery of much heavier payloads to the surface of Mars than is pos...
The Mid-Lift-to-Drag Ratio Rigid Vehicle (MRV) is a proposed candidate in the NASA Evolvable Mars Ca...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.Th...
Defining a feasible vehicle design and mission architecture capable of reliably delivering apayload ...
29th AAS Guidance and Control Conference February 2006, Breckenridge, CO.Near-term capabilities for...
As the agency space transportation lead center, Marshall Space Flight Center has been conducting tra...
IEEE Aerospace Conference March 2006, Big Sky, MT.The United States has successfully landed five r...