A new self-pressurizing propulsion system has liquid thrusters and gas jet attitude control without heavy gas storage vessels. A pump boosts the pressure of a small fraction of the hydrogen peroxide, so that reacted propellant can controllably pressurize its own source tank. The warm decomposition gas also powers the pump and is supplied to the attitude control jets. The system has been incorporated into a prototype microsatellite for terrestrial maneuvering tests. Additional progress includes preliminary testing of a bipropellant thruster, and storage of unstabilized hydrogen peroxide in small sealed tanks
The results of an experimental study of a milli-Newton high test hydrogen peroxide microthruster are...
A continuing demand exists to develop the capabilities of nanosatellites. A key element limiting the...
The goal of the research was to investigate a low cost bi-propellant engine of 40N thrust, suitable ...
Abstract. A new self-pressurizing propulsion system has liquid thrusters and gas jet attitude contro...
As satellite designs shrink, providing maneuvering and control capability falls outside the realm of...
Hydrogen peroxide tanks can be pressurized with decomposed HTP (high test hydrogen peroxide) origina...
As satellite designs shrink, providing maneuvering and control capability falls outside the realm of...
Abstract. As satellite designs shrink, providing maneuvering and control capability falls outside th...
Green propellants used for satellite-level propulsion system become attractive in recent years becau...
The ongoing developmental studies on the application of hydrogen peroxide for propulsion are briefly...
The ongoing developmental studies on the application of hydrogen peroxide for propulsion are briefly...
This paper describes the development of a lightweight high performance pump-fed divert and attitude ...
The following paper presents the key design and test activities associated with the development of P...
To increase effective load, light-weight micro-propulsion system is necessary for micro-satellites. ...
The theory, experimentation, and implementation of a green monopropellant propulsion system for smal...
The results of an experimental study of a milli-Newton high test hydrogen peroxide microthruster are...
A continuing demand exists to develop the capabilities of nanosatellites. A key element limiting the...
The goal of the research was to investigate a low cost bi-propellant engine of 40N thrust, suitable ...
Abstract. A new self-pressurizing propulsion system has liquid thrusters and gas jet attitude contro...
As satellite designs shrink, providing maneuvering and control capability falls outside the realm of...
Hydrogen peroxide tanks can be pressurized with decomposed HTP (high test hydrogen peroxide) origina...
As satellite designs shrink, providing maneuvering and control capability falls outside the realm of...
Abstract. As satellite designs shrink, providing maneuvering and control capability falls outside th...
Green propellants used for satellite-level propulsion system become attractive in recent years becau...
The ongoing developmental studies on the application of hydrogen peroxide for propulsion are briefly...
The ongoing developmental studies on the application of hydrogen peroxide for propulsion are briefly...
This paper describes the development of a lightweight high performance pump-fed divert and attitude ...
The following paper presents the key design and test activities associated with the development of P...
To increase effective load, light-weight micro-propulsion system is necessary for micro-satellites. ...
The theory, experimentation, and implementation of a green monopropellant propulsion system for smal...
The results of an experimental study of a milli-Newton high test hydrogen peroxide microthruster are...
A continuing demand exists to develop the capabilities of nanosatellites. A key element limiting the...
The goal of the research was to investigate a low cost bi-propellant engine of 40N thrust, suitable ...