“We believe the AR1 is the best, most affordable option to eliminate U.S. dependence on foreign sources of propulsion while maintaining assured access to space for our nation’s critical national security and civil space assets,” says Linda Cova, the executive director of Hydrocarbon Engine Programs at Aerojet Rocketdyne.
Cova says the AR1 is designed to integrate with the Atlas V launch vehicle and it could also serve as a versatile propulsion system for a variety of current and future launch vehicle applications.
“When you consider the minimal changes to the Atlas V launch vehicle, launch pad and related infrastructure that are required with an AR1 solution, this approach is clearly the best path toward finding a replacement for the RD-180 and meeting the launch needs of our nation,” Cova says. “We look forward to working with the U.S. government in a competitive procurement environment to bring this engine to market.”
According to the 2015 National Defense Authorization Act, alternatives like the Russian-built RD-180 must be replaced by an American-made alternative by 2019. The project began in 2014, and it’s an extension of a decade’s work on projects like the recent AFRL Hydrocarbon Boost Technology Demonstration and the NASA Advanced Booster Engineering Demonstration and Risk Reduction program.
The engine technology which drives the AR-1 has so far meant Aerojet has invested some $300 million in research and development, and the motors are expected to cost about $25 million a pair.
“Rocket engine components are complex machined pieces that require significant labor and time to produce,” says Tyler Hickman, the team lead at the NASA Glenn Research Center in Cleveland. “The injector is one of the most expensive components of an engine.”
Michael Gazarik, NASA’s associate administrator for space technology in Washington, says the agency understands that AM is “game-changing for new mission opportunities, significantly reducing production time and cost by ‘printing’ tools, engine parts or even entire spacecraft.”
The development of AR1 is currently being funded by Rocketdyne with assistance from United Launch Alliance (ULA). The single-element, main injector hot-fire tests were meant to evaluate element designs and fabrication methods for the parts, and several injectors were fabricated. The injectors were tested to pressures in excess of 2,000 psi. Aerojet Rocketdyne says these tests represent the highest pressure hot-fires of an additively-manufactured part to date.
Have you heard of any other sophisticated uses of 3D printing technology for aerospace-related applications? Let us know in the 3D Printed Rocket Engine Injectors forum thread on 3DPB.com.