A method for precision landing of manned spacecraft and cargo modules on Mars using guided parachutes was successfully demonstrated in terrestrial tests. A simulation model was developed based on those tests to explore the full capability of this type of system. The Mars Guided Parachute (MGP) concept of minimizing Mars landing site errors was found to be a practical and valuable approach. For this effort, off-the-shelf hardware was selected and assembled. Aerial drop tests were conducted on Earth at Mars-relevant atmospheric densities to collect representative performance data on how well such a system would traverse upon command to a desired landing target. A 3 degree of freedom (3 DoF) model was employed to evaluate a Mars-scaled landing...
This paper describes the system architecture and implementation approach for the Mars Pathfinder spa...
In the propulsive phase (after parachute release) of planetary landing like Mars or Moon, horizontal...
Planetary exploration has always been a very complex and risky engineering problem. Building on the ...
A key requirement for enabling Mars manned mission is the capability to land a payload within 100 m ...
A key requirement for enabling manned Mars missions is the capability to land a payload within 100 m...
Future missions to Mars may require pin-point landing precision, possibly on the order of tens of me...
The United States has successfully landed five robotic systems on the surface of Mars. These systems...
Parachutes used for Mars landing missions are only certified for deployment at Mars behind blunt bod...
A multi-body flight simulation for the Mars Smart Lander has been developed that includes six degree...
Demands for planetary landing Unmanned exploratory missions to e.g. Mars involve a landing phase, wh...
To ensure successful future Mars landing missions, the lander must be capable of detecting hazards i...
An entry, descent, and flight (EDF) trajectory profile for a Mars airplane mission is defined as con...
Mars landings at higher elevations than achieved to date are desired for scientific pursuits. The ph...
Circular parachutes have been used for aerial payload/personnel deliveries for over 100 years. In t...
Flight test of conical spacecraft simulating parachute deployment in Mars atmospher
This paper describes the system architecture and implementation approach for the Mars Pathfinder spa...
In the propulsive phase (after parachute release) of planetary landing like Mars or Moon, horizontal...
Planetary exploration has always been a very complex and risky engineering problem. Building on the ...
A key requirement for enabling Mars manned mission is the capability to land a payload within 100 m ...
A key requirement for enabling manned Mars missions is the capability to land a payload within 100 m...
Future missions to Mars may require pin-point landing precision, possibly on the order of tens of me...
The United States has successfully landed five robotic systems on the surface of Mars. These systems...
Parachutes used for Mars landing missions are only certified for deployment at Mars behind blunt bod...
A multi-body flight simulation for the Mars Smart Lander has been developed that includes six degree...
Demands for planetary landing Unmanned exploratory missions to e.g. Mars involve a landing phase, wh...
To ensure successful future Mars landing missions, the lander must be capable of detecting hazards i...
An entry, descent, and flight (EDF) trajectory profile for a Mars airplane mission is defined as con...
Mars landings at higher elevations than achieved to date are desired for scientific pursuits. The ph...
Circular parachutes have been used for aerial payload/personnel deliveries for over 100 years. In t...
Flight test of conical spacecraft simulating parachute deployment in Mars atmospher
This paper describes the system architecture and implementation approach for the Mars Pathfinder spa...
In the propulsive phase (after parachute release) of planetary landing like Mars or Moon, horizontal...
Planetary exploration has always been a very complex and risky engineering problem. Building on the ...