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A Modular Aerospike Engine Design Using Additive ManufacturingA modular aerospike engine concept has been developed with the objective of demonstrating the viability of the aerospike design using additive manufacturing techniques. The aerospike system is a self-compensating design that allows for optimal performance over the entire flight regime and allows for the lowest possible mass vehicle designs. At low altitudes, improvements in Isp can be traded against chamber pressure, staging, and payload. In upper stage applications, expansion ratio and engine envelope can be traded against nozzle efficiency. These features provide flexibility to the System Designer optimizing a complete vehicle stage. The aerospike concept is a good example of a component that has demonstrated improved performance capability, but traditionally has manufacturing requirements that are too expensive and complex to use in a production vehicle. In recent years, additive manufacturing has emerged as a potential method for improving the speed and cost of building geometrically complex components in rocket engines. It offers a reduction in tooling overhead and significant improvements in the integration of the designer and manufacturing method. In addition, the modularity of the engine design provides the ability to perform full scale testing on the combustion devices outside of the full engine configuration. The proposed design uses a hydrocarbon based gas-generator cycle, with plans to take advantage of existing powerhead hardware while focusing DDT&E resources on manufacturing and sub-system testing of the combustion devices. The major risks for the modular aerospike concept lie in the performance of the propellant feed system, the structural integrity of the additive manufactured components, and the aerodynamic efficiency of the exhaust flow.
Document ID
20140010459
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Peugeot, John
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Garcia, Chance
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Burkhardt, Wendel
(Wask Engineering Cameron Park, CA, United States)
Date Acquired
August 5, 2014
Publication Date
May 19, 2014
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M14-3275
Meeting Information
Meeting: JANNAF Propulsion Meeting
Location: Charleston, SC
Country: United States
Start Date: May 19, 2014
End Date: May 22, 2014
Sponsors: NASA Headquarters, Department of the Air Force, Department of the Army, Department of the Navy
Distribution Limits
Public
Copyright
Public Use Permitted.
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