RS-18

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RS-18
Country of origin  United States
Manufacturer Rocketdyne
Application Upper stage/Spacecraft propulsion
Predecessor Bell / Rocketdyne LMAE
Status Development
Liquid-fuel engine
Propellant LOX / Liquid Methane CH4
Cycle Pressure-fed engine
Configuration
Chamber 1
Performance
Thrust (vac.) 24.5 kN (5,500 lbf)
Used in

Development

Planned for Altair (spacecraft)


RS-18 is the Lunar Module Ascent Engine (LMAE) engine that Rocketdyne brought back out of its 36 year retirement, now designated as RS-18, and reconfigured this non-throttleable hypergolic engine to use LOX/Liquid Methane CH4 for NASA Exploration Systems Architecture Study (ESAS) engine testing in 2008.[1][2]

Development[edit]

The 2005 NASA Exploration Systems Architecture Study (ESAS) recommended that the crew exploration vehicle (CEV) lunar surface access module (LSAM) ascent stage propulsion and service module propulsion systems employ a pressure-fed LOX/Liquid Methane (CH4) technology.
"Green" propellants, such as use LOX/Liquid Methane CH4, offer savings in both performance and safety over equivalently sized hypergolic propulsion systems in spacecraft applications such as ascent engines or service module engines.[3]
The mass savings over monomethyl hydrazine (MMH) and nitrogen tetroxide N2O4 were around 1,000 - 2,000 lbm (450 – 910 kg) for the LSAM ascent module, which was larger than the current design.
The thrust levels identified in ESAS were 5,000 - 10,000 lbf (22 - 44 kN) for the ascent engine.[4]
To remove key technology risks in the decision for hypergolic or LOX/Methane, the Propulsion and Cryogenics Advanced Development (PCAD) project is being conducted within NASA, led by the Glenn Research Center, for 5,500 lbf (24,500 N) ascent engine technology.

Progress[edit]

The RS-18 rocket engine was tested using liquid oxygen (LOX) and liquid methane (LCH4) propellants under simulated altitude conditions at NASA Johnson Space Center White Sands Test Facility (WSTF). This project is part of NASA's Propulsion and Cryogenics Advanced Development (PCAD) project.
Altitude simulation was achieved using the WSTF Large Altitude Simulation System, which provided altitude conditions equivalent up to —122,000 ft (~ 37 km). The RS-18 gas spark-torch igniters were designed and supplied by Pratt and Whitney Rocketdyne as part of the LOX/Methane RS-18 test program. Pyrotechnic ignition was not attempted on the RS-18, but was subsequently successfully demonstrated as part of the 2009 Armadillo Aerospace IPP engine testing.

Main article: Altair (spacecraft)

The RS-18 engine was not selected for the Constellation program, but that NASA program was eventually cancelled on February 1, 2010.[5]

The RS-18 engine, modified to burn liquid oxygen and liquid methane through NASA's Exploration Technology Development Program, is an available and tested propulsion technology for future space exploration missions.

References[edit]

  1. ^ "New RS-18 builds upon LM Ascent Engine heritage". SpaceRef.com. September 3, 2008. 
  2. ^ "Former Moon Engine Burns Bright Once More". NASA. August 1, 2008. Retrieved June 7, 2012. 
  3. ^ Dr. Marc D. Rayman (2007-07-15). "DAWN Journal". JPL NASA. Retrieved 2008-09-06. 
  4. ^ John C. Melcher IV and Jennifer K. Allred (2008). "Liquid Oxygen / Liquid Methane Test Results of the RS-18 Lunar Ascent Engine at Simulated Altitude Conditions at NASA White Sands Test Facility". AIAA. 
  5. ^ "Fiscal Year 2011 Budget Estimates". Retrieved March 7, 2010. 

 This article incorporates public domain material from websites or documents of the National Aeronautics and Space Administration.