Add to ORKGAs HIAD technology progresses from 3-m diameter experimental scale to as large as 20-m diameter for human Mars entry, the mass penalties of carrying compressed gas has led the HIAD team to research current state-of-the-art gas generator approaches. Summarized below are several technologies identified in this survey, along with some of the pros and cons with respect to supporting large-scale HIAD applications
To support NASAs long term goal of landing humans on Mars, technologies which enable the landing of ...
The minimum inflation pressure and volume are key characteristics of an IAD design because the mass ...
A high-strength, low-weight pressure vessel dome was designed specifically to house a high-pressure ...
Hypersonic Inflatable Aerodynamic Decelerator (HIAD) technology readiness levels have been increment...
Over a decade of work has been conducted in the development of NASAs Hypersonic Inflatable Aerodynam...
This paper explores the impact of human Mars mission architecture decisions on the design and perfor...
The successful flight of the Inflatable Reentry Vehicle Experiment (IRVE)-3 has further demonstrated...
To support NASAs long term goal of landing humans on Mars, technologies which enable the landing of ...
The use of inflatable space structures has often been proposed for aerospace and planetary applicati...
To make the most of ridesharing opportunities, small satellite (SmallSat) mission designers endeavor...
A gas-generating device was developed to supplement the ram-air inflation of a supersonic ballute. T...
The preliminary design of a counterrotating fast discharge homopolar generator (HPG) and a counterro...
Inert gases are of interest as possible alternatives to the usual electric thruster propellants of m...
Cool Gas Generators are an innovative means to store gas which can be used in propulsion and pressur...
Over a decade of work has been conducted in the development of NASA's Hypersonic Inflatable Aerodyna...
To support NASAs long term goal of landing humans on Mars, technologies which enable the landing of ...
The minimum inflation pressure and volume are key characteristics of an IAD design because the mass ...
A high-strength, low-weight pressure vessel dome was designed specifically to house a high-pressure ...
Hypersonic Inflatable Aerodynamic Decelerator (HIAD) technology readiness levels have been increment...
Over a decade of work has been conducted in the development of NASAs Hypersonic Inflatable Aerodynam...
This paper explores the impact of human Mars mission architecture decisions on the design and perfor...
The successful flight of the Inflatable Reentry Vehicle Experiment (IRVE)-3 has further demonstrated...
To support NASAs long term goal of landing humans on Mars, technologies which enable the landing of ...
The use of inflatable space structures has often been proposed for aerospace and planetary applicati...
To make the most of ridesharing opportunities, small satellite (SmallSat) mission designers endeavor...
A gas-generating device was developed to supplement the ram-air inflation of a supersonic ballute. T...
The preliminary design of a counterrotating fast discharge homopolar generator (HPG) and a counterro...
Inert gases are of interest as possible alternatives to the usual electric thruster propellants of m...
Cool Gas Generators are an innovative means to store gas which can be used in propulsion and pressur...
Over a decade of work has been conducted in the development of NASA's Hypersonic Inflatable Aerodyna...
To support NASAs long term goal of landing humans on Mars, technologies which enable the landing of ...
The minimum inflation pressure and volume are key characteristics of an IAD design because the mass ...
A high-strength, low-weight pressure vessel dome was designed specifically to house a high-pressure ...