Written by Tracy McMahan/Kimberly Newton
NASA Marshall Space Flight Center
Huntsville, AL – NASA has tested a 3-D printed rocket engine turbopump with liquid methane – an ideal propellant for engines needed to power many types of spacecraft for NASA’s journey to Mars.
“This is one of the most complex rocket parts NASA has ever tested with liquid methane, a propellant that would work well for fueling Mars landers and other spacecraft,” said Mary Beth Koelbl, the manager of the Propulsions Systems Department at NASA’s Marshall Space Flight Center in Huntsville, Alabama.
“Additive manufacturing, or 3-D printing, made it possible to quickly design, build and test two turbopumps with identical designs that worked well with both liquid methane and liquid hydrogen propellant,” stated Koelbl.
A turbopump is complex because it has turbines that spin fast to drive the pump, which supplies fuel to the engine.
During the full power test, the turbines generated 600 horsepower and the fuel pump, got its “heartbeat” racing at more than 36,000 revolutions per minute delivering 600 gallons of semi-cryogenic liquid methane per minute – enough to fuel an engine producing over 22,500 pounds of thrust. Three other tests were completed at lower power levels.
These tests along with manufacturing and testing of injectors and other rocket engine parts are paving the way for advancements in 3-D printing of complex rocket engines and more efficient production of future spacecraft including methane-powered landers.
“Methane propulsion and additive manufacturing are key technologies for the future of exploration including NASA’s journey to Mars,” said Graham Nelson, a Marshall propulsion engineer who helped with the testing. “We’re excited to complete testing that advances both these technologies at the same time and improves the capabilities of future missions.”
Liquid methane is cooled to 255 degrees below zero Fahrenheit (-159 degrees Celsius) whereas liquid hydrogen is cooled to 400 degrees below zero Fahrenheit (-240 degrees Celsius).
The higher temperature of liquid methane means it boils off more slowly and thus is easier to store for longer periods, a benefit for Mars missions.
“By demonstrating the same turbopump can work with different fuels, we’ve shown that a common design would work for either engines fueled by methane or hydrogen,” said Marty Calvert, the Marshall engineer who designed the turbopump. “Because liquid methane is much more dense than hydrogen, it requires the turbopump to spin at a different speed to deliver the same amount of mass flow to the engine.”
Testing ensures 3-D printed parts operate successfully under conditions similar to those in landers, ascent vehicles and other space vehicles. Test data are available to American companies working to drive down the cost of using this new manufacturing process to build parts that meet aerospace standards.
All data on materials characterization and performance are compiled in NASA’s Materials and Processes Technical Information System, called MAPTIS, which is available to approved users.
“Additive manufacturing allowed us to build the turbopump with 45 percent fewer parts,” said Nick Case, the Marshall propulsion engineer who led the testing. “This made it affordable to build two turbopumps, get them on the test stand quickly, and get results. Our next step will be to test the liquid methane turbopump with other 3-D printed engine components in a similar configuration to the liquid hydrogen tests completed last year.”