Design of an Advanced Expander Test BedThe final design of the Advanced Expander Test Bed (AETB) is discussed. The AETB is a cryogenic rocket ground test unit being designed and built for NASA to enable validation of mission-focused technologies for advanced space engines. Based on the split expander cycle, it will operate at a nominal thrust of 20,000 lbf, a chamber pressure of 1200 psia, and may be operated off-design over a wide range of throttling conditions and mixture ratios. The design approach and configuration of the major components are described.
Document ID
19930065955
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mitchell, John C. (Pratt & Whitney Group West Palm Beach, FL, United States)
Tabata, William K. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
AIAA PAPER 93-2133
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit