Miniaturized hypergolic bipropellant thruster delivering 3 N thrust at 285 s Isp, developed for a NASA-funded deep-space nanosatellite mission.
Nanosatellite Mono & Bipropellant Propulsion Thruster
Miniaturized hypergolic bipropellant thruster delivering 3 N thrust at 285 s Isp, developed for a NASA-funded deep-space nanosatellite mission.
Description
As part of early R&D for a NASA-funded deep space nano-satellite mission, Stellar Exploration designed, built, and tested a miniaturized hypergolic bipropellant thruster. It provides 3 N of thrust with 285 seconds of specific impulse. Propellant is pressurized with gear pumps, allowing for precise propellant metering and a low-pressure tank design. The in-house propulsion system controller board design leverages state-of-the-art BLDC motor control, and includes hardware for all necessary sensors and actuators.
Stellar Exploration also produces monopropellant thrusters in 0, 45 and 90 degree configurations, which have been extensively hot-fire tested. The company designed, built, and delivered the full propulsion system for NASA's 12U CAPSTONE mission to the Moon, and separately built the propulsion system for EchoStar's EG-3 satellite, completed in nine months, which achieved approximately 65 m/s of delta-V post-launch (a small-satellite world record at the time) with roughly 485 m/s of propellant remaining for subsequent maneuvers and deorbiting.
The company is currently developing propulsion systems for Mars-bound ESPA-class satellites, highly maneuverable DoD constellations, and in-space refueling technology.
Specifications
| Thrust | 3 N |
|---|---|
| Specific impulse | 285 sec |
| Propellant feed | Gear pumps for precise propellant metering, low-pressure tank design |
| Propellant type | Hypergolic bipropellant; monopropellant variants also available |
| Flight heritage | NASA CAPSTONE (12U lunar mission), EchoStar EG-3 (small-satellite delta-V record) |