This work presents studies and analysis in support of a Mars Ascent Vehicle as part of a Martian Sample Return campaign. The vehicle design has been ongoing, with rapid development of a 6 Degree of Freedom simulation to capture full vehicle dispersions and integrated performance of vehicle, guidance, navigation and control. The maturation of this simulation is presented to provide an overview of its capabilities added over the past year of effort. The results describe in detail guidance algorithm development to increase the systems robustness to thrust sensitivities. Navigation performance and sensitivity analysis are included to describe the capabilities of the current design as well as identify primary drivers of insertion performance. La...
An advanced guidance algorithm, Fully Numerical Predictor-corrector Aerocapture Guidance (FNPAG), ha...
Future Mars exploration missions, both robotic and piloted, may utilize Earth to Mars transfer traje...
Several international missions scheduled for years 2011--2013 have as objective a Mars surface sampl...
This paper focuses on the work being performed at the NASA Marshall Space Flight Center (MSFC) in su...
To support development of Martian Ascent Vehicles, analysis tools are needed to support the developm...
Human Mars mission architecture studies have shown that the ascent vehicle mass drives performance r...
Recent trades have taken place on solid propulsion options to support a potential Mars Sample Retrie...
The Mid-Lift-to-Drag ratio Rigid Vehicle (MRV) is a candidate in the NASA multi-center effort to det...
Mars landings at higher elevations than achieved to date are desired for scientific pursuits. The ph...
Future missions to Mars may require pin-point landing precision, possibly on the order of tens of me...
Astronauts on a mission to Mars will require several vehicles working together to get to Mars orbit,...
One challenge driving Mars entry, descent and landing technology development is to land at higher el...
Problems related to an unmanned exploration of the planet Mars by means of an autonomous roving plan...
In an effort to mature the design of the Mid-Lift-to-Drag ratio Rigid Vehicle (MRV) candidate of the...
Precision landing on Mars is a challenge. All Mars lander missions prior to the 2012 Mars Science La...
An advanced guidance algorithm, Fully Numerical Predictor-corrector Aerocapture Guidance (FNPAG), ha...
Future Mars exploration missions, both robotic and piloted, may utilize Earth to Mars transfer traje...
Several international missions scheduled for years 2011--2013 have as objective a Mars surface sampl...
This paper focuses on the work being performed at the NASA Marshall Space Flight Center (MSFC) in su...
To support development of Martian Ascent Vehicles, analysis tools are needed to support the developm...
Human Mars mission architecture studies have shown that the ascent vehicle mass drives performance r...
Recent trades have taken place on solid propulsion options to support a potential Mars Sample Retrie...
The Mid-Lift-to-Drag ratio Rigid Vehicle (MRV) is a candidate in the NASA multi-center effort to det...
Mars landings at higher elevations than achieved to date are desired for scientific pursuits. The ph...
Future missions to Mars may require pin-point landing precision, possibly on the order of tens of me...
Astronauts on a mission to Mars will require several vehicles working together to get to Mars orbit,...
One challenge driving Mars entry, descent and landing technology development is to land at higher el...
Problems related to an unmanned exploration of the planet Mars by means of an autonomous roving plan...
In an effort to mature the design of the Mid-Lift-to-Drag ratio Rigid Vehicle (MRV) candidate of the...
Precision landing on Mars is a challenge. All Mars lander missions prior to the 2012 Mars Science La...
An advanced guidance algorithm, Fully Numerical Predictor-corrector Aerocapture Guidance (FNPAG), ha...
Future Mars exploration missions, both robotic and piloted, may utilize Earth to Mars transfer traje...
Several international missions scheduled for years 2011--2013 have as objective a Mars surface sampl...