Multimode Chemical-Electric Propulsion Transfer Stage for Flexible Cislunar Operations

Project Details

Description

The innovation is a multimode chemical-electric propulsion equipped transfer stage for venture class small launch vehicles that is flexible and adaptable to meet a wide range of NASA lunar mission needs and requirements.nbsp;This innovation is enabled by a novel space propulsion system that combines chemical and electric propulsion with shared propellant between the modes (multimode propulsion, MMP).nbsp; Through previous efforts, we have developed technologies that enable this type of system. This includes development of our electrosprayable lsquo;greenrsquo; monopropellants FAM-110A and FAM-122A, demonstration of chemical and electric thrusters using these monopropellants, and development of a propellant feed system capable of supplying the three order of magnitude difference in flow rates required for operation in either mode. This project will demonstrate a 22 N chemical monopropellant thruster using our FAM-122A monopropellant, designed for inclusion as the main engine in a transfer stage capable of injecting a 25 kg small satellite payload into a TLI orbit from a small venture class launch vehicle using only chemical propulsion. The transfer stage systems, however, will also accomodate our feed system and electrospray thrusters, initially used for purposes of minor course correction, pointing, and disposal maneuvers. As electrospray technology matures, upgraded thrusters can be swapped into the vehicle to enable missions to Mars, Venus, and near Earth asteroids.nbsp;This project will also perform small scale hazard classification tests, data from which will be used to assignnbsp;a DOT 1.3 interim classification by the conclusion of the project in addition to investigation and development of production scale up plans.

StatusFinished
Effective start/end date7/22/221/25/23

Funding

  • National Aeronautics and Space Administration: $137,090.00

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