XLR40-RM-2 SUPERPERFORMANCE TURBOROCKET PROPULSION SYSTEM DEVELOPMENT

1956 ◽  
Author(s):  
Jr Burdett ◽  
H. W.
Keyword(s):  
System Development ◽  
Propulsion System

Status of Ion Propulsion System Development at Aerojet Redmond

2003 ◽  
Author(s):  
Fred Wilson ◽  
W. Andrew Hoskins ◽  
Randall Aadland ◽  
Jeffrey Monheiser ◽  
Nicole Meckel ◽  
...  
Keyword(s):  
System Development ◽  
Propulsion System ◽  
Ion Propulsion

scholarly journals STSAT-3 Hall Thruster Propulsion System Development

2010 ◽  
Vol 38 (8) ◽  
pp. 834-841 ◽  
Author(s):  
Hee-Keun Cho ◽  
Kwang-Sun Ryu ◽  
Won-Ho Cha ◽  
Jong-Sup Lee ◽  
Mi-Hee Seo ◽  
...  
Keyword(s):  
System Development ◽  
Propulsion System ◽  
Hall Thruster

XFV-12A Propulsion System Development

1976 ◽  
Author(s):  
J. T. Delany ◽  
G. M. Jenkins
Keyword(s):  
System Design ◽  
Development Process ◽  
System Development ◽  
Full Scale ◽  
Propulsion System ◽  
Design And Development ◽  
Plug Nozzle ◽  
Design Philosophy ◽  
Thrust System ◽  
Testing And Evaluation

The XFV-12A total powered lift/thrust system being developed under contract for the U. S. Navy is described. The description includes design and development to date of the inlets, engine integration, the diverter valve with plug nozzle, the lift system augmenter supply ducting, and lift/thrust augmenter hardware. The development process description includes system design philosophy and criteria, analysis, test facilities utilized, model and full-scale testing and evaluation.

Overview of Ion Propulsion System Development at Aerojet Redmond

2004 ◽  
Author(s):  
Fred Wilson ◽  
Andy Hoskins ◽  
Jeff Monheiser ◽  
Nicole Meckel ◽  
Randy Aadland ◽  
...  
Keyword(s):  
System Development ◽  
Propulsion System ◽  
Ion Propulsion
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