<p>This thesis focuses on the development of reduced pressure
testing capabilities at Zucrow Laboratories.
A two-stage ejector on loan from NASA Marshall is used in series with a
supersonic diffuser to allow for the testing of up to100 lb<sub>f</sub> rocket
engines at equivalent altitudes of up to 100,000 ft. The objective of this research is to
implement a one-dimensional (1-D) model which accurately predicts the
performance of the two-stage ejector in real time, informing the maximum thrust
and simulated altitude capabilities within the altitude chamber located in room
134A of ZL3 during experimental testing.</p>
| Identifer | oai:union.ndltd.org:purdue.edu/oai:figshare.com:article/9108356 |
| Date | 15 August 2019 |
| Creators | Jacob M McCormick (7043039) |
| Source Sets | Purdue University |
| Detected Language | English |
| Type | Text, Thesis |
| Rights | CC BY 4.0 |
| Relation | https://figshare.com/articles/Design_and_Characterization_of_an_Altitude_Chamber_for_Chemical_Rocket_Engines/9108356 |
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