Temperature Jump Pyrolysis Studies Of Rp-2 Fuel
Abstract
This paper explores the pyrolysis of RP-2, a rocket fuel derived from kerosene, on different catalytic surfaces relevant to endothermic cooling applications used in rockets. RP-2 fuel formulations contain thousands of compounds some of which breakdown at high temperatures by absorbing heat and sometimes form carbon deposits (coking). Thus the pyrolysis chemistry of RP-2 is an intense research topic. Here, Rapid Scan Fourier-TransformIinfrared (RS-FTIR) spectroscopy was used to measure the products of pyrolysis on different materials. The maximum temperature for the experiments was 800 °C with a temperature rise rate of 600 °C per second. Pressure in the chamber ranged from 5 to up to 25 atm. The materials chosen for the present experiments were nichrome and pure copper. The results show that pyrolysis products have a strong dependence on pressure.
Publication Date
1-1-2017
Publication Title
AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
Document Type
Article; Proceedings Paper
Personal Identifier
scopus
DOI Link
https://doi.org/10.2514/6.2017-0611
Copyright Status
Unknown
Socpus ID
85017277429 (Scopus)
Source API URL
https://api.elsevier.com/content/abstract/scopus_id/85017277429
STARS Citation
Pryor, Owen M.; Chambreau, Steven D.; Vaghjiani, Ghanshyam L.; and Vasu, Subith, "Temperature Jump Pyrolysis Studies Of Rp-2 Fuel" (2017). Scopus Export 2015-2019. 6898.
https://stars.library.ucf.edu/scopus2015/6898