Small-Scale Hybrid Rocket Test Stand & Characterization of Swirl Injectors
abstract: Derived from the necessity to increase testing capabilities of hybrid rocket motor (HRM) propulsion systems for Daedalus Astronautics at Arizona State University, a small-scale motor and test stand were designed and developed to characterize all components of the system. The motor is desig...
Other Authors: | Summers, Matt H. (Author) |
---|---|
Format: | Dissertation |
Language: | English |
Published: |
2013
|
Subjects: | |
Online Access: | http://hdl.handle.net/2286/R.I.18089 |
Similar Items
-
Design and Testing of Digitally Manufactured Paraffin Acrylonitrile-Butadiene-Styrene Hybrid Rocket Motors
by: McCulley, Jonathan M.
Published: (2013) -
Throttleable GOX/ABS Launch Assist Hybrid Rocket Motor for Small Scale Air Launch Platform
by: Spurrier, Zachary S.
Published: (2016) -
Direct Electrical Arc Ignition of Hybrid Rocket Motors
by: Judson, Michael I., Jr.
Published: (2015) -
A Study of the Characteristics of Gas-On-Liquid Impinging Injectors
by: Rakesh, P
Published: (2018) -
Experimental Study on the Discharge Coefficient of Bi-Swirl Coaxial Injectors
by: K. Ahn, et al.
Published: (2019-01-01)