The Flight Works team is proud to have worked with NASA, Plasma Processes, and GA Tech on the Lunar Flashlight Propulsion system.
Flight Works to attend the 35th annual Small Sat Conference which will be held virtually August 7th-12th 2021. Known in the space industry as the premier conference on small satellites, the conference is expected to bring the brightest minds together to network and discuss the past year’s successes, current challenges, as well as share innovative technological advances in small spacecraft development.
A Flight Works propellant pump will play a critical role in Stellar Exploration’s propulsion system on NASA’s CAPSTONE CubeSat. NASA’s Cislunar Autonomous Positioning System Technology Operations and Navigation Experiment (CAPSTONE) is a 55-pound spacecraft that will launch later in 2021 and take three months to arrive at its destination, to orbit around the moon for another six months. CAPSTONE’s primary objective is to test and verify the calculated orbital stability of a Near Rectilinear Halo Orbits (NRHO) around the moon. This will help reduce risk for future spacecraft and NASA’s planned Gateway Lunar outpost, a small space station that will orbit around the moon to provide astronauts with access to the lunar surface.
Flight Work’s President and CEO, Eric Besnard joined Maxon’s Robin Phillips as guest speakers on a Tech Briefs webinar discussing the topic of Customizing Actuators Using COTS Drive Components for Martian Mission Mechanisms. You can listen to a recording of the webinar at the link below.
Flight Works is proud to support the NASA Lunar Flashlight Mission. Flight Work’s propellant pump is to be used in the propulsion system aboard NASA’s Lunar Flashlight, a small satellite, or CubeSat, slated to launch as a secondary satellite on the Artemis mission in the fall of 2021. (more…)
As part of a NASA Phase I SBIR, Flight Works is expanding its micropump-fed propulsion technology to the development and demonstration of a low cost, compact, high performance lunar transfer stage designed for small launchers like Rocket Lab’s Electron and Virgin Orbit’s Launcher One. With a total wet mass around 230 kg, the transfer stage (more…)
Project managed by the Jet Propulsion Laboratory (JPL)
Flight Works will expand its work in micro gear pumps for propulsion applications in order to provide a highly capable propulsion and attitude control system (ACS) for asteroid proximity operations, landers and return capsules.
Flight Works is proposing to expand its work in micro gear pumps for propulsion applications in order to provide a highly capable propulsion and attitude control system (ACS) for asteroid proximity operations, landers and return capsules. In traditional systems, larger thrusters, specific to each mission, must be employed to counter the gravity field of the target. Also, throttling these larger thrusters for proximity operations and landing is not a trivial task. With the pump, the need for these larger, more expensive thrusters is eliminated. Instead the pump allows increasing (or decreasing) and controlling the thrust of the attitude control thrusters to the levels required for operating in the target’s gravity field by modulating the pump RPM/power. Typically, only a few tens of watts are needed for pump operations. Flight Works is prepared to develop and demonstrate a low cost micro pump capable of significantly increasing pressure and flow rate to the thrusters, to define a roadmap for larger increases if warranted, and to plan Phase II activities in order to reach a TRL 7 by the end of that phase. The technology builds on Aerojet Rocketdyne’s work for NASA’s on-going Green Propellant Infusion Mission (GPIM) and use the non-toxic hydroxyl ammonium-nitrate (HAN) -based propellant AF-M315E which provides 50% greater density-ISP than hydrazine. The micro pump leverages the Air Force Research Lab’s (AFRL) investments in pump-fed technologies for small spacecraft propulsion applications, which have led to steady state and pulsed hot fire tests with hydrazine and demonstrations with other propellants.
Flight Works releases a family of ultra-low flow pumps capable of controlling flow rates under 1 mL/min.
Flight Works releases a new family of ultra-low flow pumps capable of maintaining accurate flow rates under 1 mL/min. Using the smallest internal components yet entered into production at Flight Works, this design facilitates high-speed and high-torque operation without excess flow rate, allowing for nominal motor operation and relatively high differential pressures. With testing conducted into the microliters, and as high as 10 bars of differential pressure with low viscosity fluids, Flight Works has verified this configuration as an excellent solution for a wide range of low-flow requirements.
Though Flight Works already excelled in the low-flow sector, these new models are an improved fit for a number of uses. Primary target markets include: