Advanced Electric Propulsion System

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The Advanced Electric Propulsion System qualification thruster inside one of the vacuum chambers at NASA Glenn's Electric Propulsion and Power Laboratory. AEPS at NASA Glenn.jpg
The Advanced Electric Propulsion System qualification thruster inside one of the vacuum chambers at NASA Glenn’s Electric Propulsion and Power Laboratory.

Advanced Electric Propulsion System (AEPS) is a solar electric propulsion system for spacecraft that is being designed, developed and tested by NASA and Aerojet Rocketdyne for large-scale science missions and cargo transportation. [1] The first application of the AEPS is to propel the Power and Propulsion Element (PPE) of the Lunar Gateway, [1] to be launched no earlier than 2025. [2] The PPE module is built by Maxar space solutions in Palo Alto, California. Two identical AEPS engines would consume 25 kW being generated by the roll-out solar array (ROSA) assembly, which can produce over 60 kW of power. [1]

Contents

The Power and Propulsion Element (PPE) for the Lunar Gateway will have a mass of 8-9 metric tons and will be capable of generating 50 kW [3] of solar electric power for its Hall-effect thrusters for maneuverability, which can be supported by chemical monopropellant thrusters for high-thrust attitude control maneuvers. [4]

Overview

Solar-electric propulsion has been shown to be reliable and efficient, and allows a significant mass reduction of spacecraft. High-power solar electric propulsion is a key technology that has been prioritized because of its significant exploration benefits in cis-lunar space and crewed missions to Mars. [1]

The AEPS Hall thruster system was originally developed since 2015 by NASA Glenn Research Center and the Jet Propulsion Laboratory to be used on the now canceled Asteroid Redirect Mission. Work on the thruster did not stop following the mission cancellation in April 2017 because there is demand of such thrusters for a range of NASA, defense and commercial missions in deep space. [1] [5] [6] Since May 2016, [7] further work on AEPS has been transitioned to Aerojet Rocketdyne that is currently designing and testing the engineering-model hardware. [1] This is a contract worth $65 million, where Aerojet Rocketdyne developed, qualified and will deliver five 12.5 kW Hall thruster subsystems, including thrusters, PPUs and xenon flow controllers. [8]

Design

AEPSPerformance [9]
Max. power consumption40 kW
Max. operating current≤ 25 A
VoltageInput: 95 V – 140V
Output: 300 V –600 V
Max. specific impulse (Isp)2,900 s
Max. thrust 600 mN /engine
Theoretical total thrust 2.356 N
Actual thrust @ 40 kW1.77 N
Distance range from Sun0.8 to 1.7 AU
System mass100 kg × 4 engines
Xenon propellant mass
(Lunar Gateway)		5,000 kg

AEPS is based on the 12.5 kW development model thruster called 'Hall Effect Rocket with Magnetic Shielding' (HERMeS). The AEPS solar electric engine makes use of the Hall-effect thruster in which the propellant is ionized and accelerated by an electric field to produce thrust. To generate 12.5 kW at the thruster actually takes a total of 13.3 kW including power needed for the control electronics. Four identical AEPS engines (thruster and control electronics) would theoretically need 4 × 13.3 kW = 53.2 kW, more than the 50 kW generated by solar panels of the PPE. [1] It is stated that the AEPS array is intended only to use 40 kW of the 50 kW, so the maximum thrust would be limited to around 1.77 N.

The engineering model is undergoing various vibration tests, thruster dynamic and thermal environment tests in 2017. [1] AEPS is expected to accumulate about 5,000 h by the end of the contract and the design aims to achieve a flight model that offers a half-life of at least 23,000 hours [1] and a full life of about 50,000 hours. [6]

The three main components of the AEPS propulsion engine are: a Hall-effect thruster, Power Processor Unit (PPU), and the Xenon Flow Controller (XFC). The thrusters are throttleable over an input power range of 6.67 –40 kW with input voltages ranging from 95 to 140 V. [1] The estimated xenon propellant mass for the Lunar Gateway would be 5,000 kg. [1] The Preliminary Design Review took place in August 2017. [10] It was concluded that "The Power Processing Unit successfully demonstrated stable operation of the propulsion system and responded appropriately to all of our planned contingency scenarios." [11]

Tests

A view from inside the vacuum chamber showing the Advanced Electric Propulsion System fired up during qualification testing at NASA Glenn. AEPS during operation.jpg
A view from inside the vacuum chamber showing the Advanced Electric Propulsion System fired up during qualification testing at NASA Glenn.

In July 2017, AEPS was tested at Glenn Research Center. [12] The tests used a Power Processing Unit (PPU), which could also be used for other advanced spacecraft propulsion technology. [12] In August 2018, Aerojet Rocketdyne completed the early systems integration test in a vacuum chamber, leading to the design finalization and verification phase. [13] [14] In November 2019, Aerojet Rocketdyne demonstrated the AEPS thruster at full power for the first time. [15] In July 2023, NASA and Aerojet Rocketdyne began qualification testing on AEPS. [16]

See also

Related Research Articles

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<span class="mw-page-title-main">Hall-effect thruster</span> Type of electric propulsion system

In spacecraft propulsion, a Hall-effect thruster (HET) is a type of ion thruster in which the propellant is accelerated by an electric field. Hall-effect thrusters are sometimes referred to as Hall thrusters or Hall-current thrusters. Hall-effect thrusters use a magnetic field to limit the electrons' axial motion and then use them to ionize propellant, efficiently accelerate the ions to produce thrust, and neutralize the ions in the plume. The Hall-effect thruster is classed as a moderate specific impulse space propulsion technology and has benefited from considerable theoretical and experimental research since the 1960s.

<span class="mw-page-title-main">Ion thruster</span> Spacecraft engine that generates thrust by generating a jet of ions

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<span class="mw-page-title-main">SMART-1</span> European Space Agency satellite that orbited the Moon

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<span class="mw-page-title-main">Aerojet Rocketdyne</span> American aerospace propulsion manufacturer

Aerojet Rocketdyne is a subsidiary of American defense company L3Harris Technologies that manufactures rocket, hypersonic, and electric propulsive systems for space, defense, civil and commercial applications. Aerojet traces its origins to the General Tire and Rubber Company established in 1915, while Rocketdyne was created as a division of North American Aviation in 1955. Aerojet Rocketdyne was formed in 2013 when Aerojet and Pratt & Whitney Rocketdyne were merged, following the latter's acquisition by GenCorp from Pratt & Whitney. On April 27, 2015, the name of the holding company, GenCorp Inc., was changed to Aerojet Rocketdyne Holdings, Inc. Aerojet Rocketdyne Holdings was acquired by L3Harris in July 2023 for $4.7 billion.

<span class="mw-page-title-main">Solar electric propulsion</span> High efficiency engine for space travel

Solar electric propulsion (SEP) refers to the combination of solar cells and electric thrusters to propel a spacecraft through outer space. This technology has been exploited in a variety of spacecraft designs by the European Space Agency (ESA), the JAXA, Indian Space Research Organisation (ISRO) and NASA. SEP has a significantly higher specific impulse than chemical rocket propulsion, thus requiring less propellant mass to be launched with a spacecraft. The technology has been evaluated for missions to Mars.

Aerojet was an American rocket and missile propulsion manufacturer based primarily in Rancho Cordova, California, with divisions in Redmond, Washington, Orange and Gainesville in Virginia, and Camden, Arkansas. Aerojet was owned by GenCorp. In 2013, Aerojet was merged by GenCorp with the former Pratt & Whitney Rocketdyne to form Aerojet Rocketdyne.

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<span class="mw-page-title-main">NASA Solar Technology Application Readiness</span> Space propulsion system, electrostatic gridded ion thruster

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<span class="mw-page-title-main">Lunar Gateway</span> Lunar orbital space station under development

The Lunar Gateway, or simply Gateway, is the first planned extraterrestrial space station. It will be placed in lunar orbit and is intended to serve as a solar-powered communication hub, science laboratory, and short-term habitation module for government-agency astronauts, as well as a holding area for rovers and other robots. It is a multinational collaborative project involving four of the International Space Station partner agencies: NASA, European Space Agency (ESA), Japan Aerospace Exploration Agency (JAXA), and Canadian Space Agency (CSA). It is planned to be both the first space station beyond low Earth orbit and the first space station to orbit the Moon.

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References

  1. 1 2 3 4 5 6 7 8 9 10 11 Overview of the Development and Mission Application of the Advanced Electric Propulsion System (AEPS). (PDF). Daniel A. Herman, Todd A. Tofil, Walter Santiago, Hani Kamhawi, James E. Polk, John S. Snyder, Richard R. Hofer, Frank Q. Picha, Jerry Jackson and May Allen. NASA; NASA/TM—2018-219761. 35th International Electric Propulsion Conference. Atlanta, Georgia, October 8–12, 2017. Accessed: 27 July 2018.
  2. ↑ Dunbar, Brian (December 18, 2023). "Gateway". NASA. Retrieved December 25, 2023.
  3. ↑ NASA issues study contracts for Deep Space Gateway element. Jeff Foust, Space News. 3 November 2017.
  4. ↑ Chris Gebhardt (April 6, 2017). "NASA finally sets goals, missions for SLS – eyes multi-step plan to Mars". NASA Spaceflight. Retrieved April 9, 2017.
  5. ↑ Jeff Foust (June 14, 2017). "NASA closing out Asteroid Redirect Mission". Space News. Retrieved September 9, 2017.
  6. 1 2 Aerojet Rocketdyne Signs Contract to Develop Advanced Electric Propulsion System for NASA. Aerojet Rocketdyne. Press release, 28 April 2016. Accessed: 27 July 2018.
  7. ↑ NASA Works to Improve Solar Electric Propulsion for Deep Space Exploration. NASA News. April 19, 2016. Accessed 27 July 2018.
  8. ↑ Aerojet Rocketdyne Successfully Tests Advanced Electric Propulsion System to Further Nation's Space Technology Capabilities. Aerojet Rocketdyne. 6 July 2017.
  9. ↑ Status of Advanced Electric Propulsion Systems for Exploration Missions. R. Joseph Cassady, Sam Wiley, Jerry Jackson. Aerojet Rocketdyne. 16 November 2018.
  10. ↑ 13kW Advanced Electric Propulsion Flight System Development and Qualification. (PDF). Jerry Jackson, May Allen, Roger Myers, Erich Soendker, Benjamin Welander, Artie Tolentino, Chris Sheehan, Joseph Cardin, John Steven Snyder, Richard R. Hofer, Todd Tofil1, Dan Herman, Sam Hablitze and Chyrl Yeatts. The 35th International Electric Propulsion Conference. Atlanta, Georgia, USA. October 8 – 12, 2017.
  11. ↑ Advanced Electric Propulsion System successfully tested at NASA's Glenn Research Center. Jason Rhian, Spaceflight Insider. 8 July 2017.
  12. 1 2 "Advanced Electric Propulsion System successfully tested at NASA's Glenn Research Center - SpaceFlight Insider". www.spaceflightinsider.com. July 8, 2017. Retrieved July 28, 2018.
  13. ↑ Successful testing gives NASA's Advanced Electric Propulsion System a boost. David Szondy, New Atlas. 29 August 2018.
  14. ↑ Aerojet Rocketdyne demonstrates advanced electric propulsion capabilities. Space Daily. 29 August 2018.
  15. ↑ "Advanced Electric Propulsion Thruster for NASA's Gateway Achieves Full Power Demonstration – Parabolic Arc". November 9, 2019. Retrieved November 11, 2019.
  16. ↑ NASA, Aerojet Rocketdyne Put Gateway Thruster System to the Test. NASA. July 12, 2023. Accessed 12 July 2023.
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