35th Joint Propulsion Conference and Exhibit 1999
DOI: 10.2514/6.1999-2599
|View full text |Cite
|
Sign up to set email alerts
|

Development and test of an advanced expander combustor

Abstract: ABSTRACTprogram. The Advanced Expander Combustor is designed to provide increased heat pick-up to the coolant and improved system thrust to weight, increased specific impulse, and increased reliability. These benefits will be accomplished and demonstrated through design, development, and test of this high heat flux, compact thrust chamber capable of supporting a chamber pressure of 1375 psia (97 kg/cm^2) in an cm* expander cycle configuration.

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
0
0

Year Published

2000
2000
2000
2000

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
references
References 0 publications
0
0
0
Order By: Relevance