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An Experimental Investigation of Hypergolic Ignition Delay of Hydrogen Peroxide with Fuel MixturesAn experimental investigation of hypergolicity and ignition delay of fuel mixtures with hydrogen peroxide is presented. Example results of high speed photography and schleiren from drop tests are shown. Also, a discussion of the sensitivity to experimental parameters such as drop size and subsequent uncertainty considerations of ignition delay results is presented. It is shown that using the described setup on the mixtures presented, the precision uncertainty is on the order of 6% of average ignition delay and 5% of average decomposition delay. This represents sufficient repeatability for first order discrimination of ignition delay for propellant development and screening. Two mixtures, each using commonly available amines and transition metal compounds, are presented as examples that result in ignition delays on the order of 10 milliseconds.
Document ID
20040027573
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Blevins, John A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Gostowski, Rudy
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Chianese, Silvio
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Propellants And Fuels
Report/Patent Number
AIAA Paper 2004-1335
Report Number: AIAA Paper 2004-1335
Meeting Information
Meeting: 42nd AIAA Aerospace Sciences Meeting
Location: Reno, NV
Country: United States
Start Date: January 5, 2004
End Date: January 8, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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