RP2-1 POSF7688
RP2 (Rocket Propellent 2) is a highly refined kerosene used as a rocket fuel.
Table I. Key properties [1].
Property |
Value |
Average formula |
C12.0H24.1 |
H/C ratio (mole) |
2.01 |
Average molecular weight (g/mol) |
167.9 |
LHV (MJ/kg) |
43.6 |
Model formula* |
C12H24 |
* For modeling purpose, it is necessary to use integer formula due to computer code limitation. For modeling purpose, use the fuel mass fraction, rather than the mole fraction [2].
Table II. Fuel composition [2].
Type |
Mass % |
n-paraffin |
2.4 |
iso-paraffin |
36.6 |
cycloparaffin |
60.7 |
aromatics |
0.3 |
others |
0 |
References
[1] M. Billingsley, personal communication, 2015.
[2] R. Xu, K. Wang, S. Banerjee, J. Shao, T. Parise, Y. Zhu, S. Wang, A. Movaghar, D.J. Lee, R. Zhao, X. Han, Y. Gao, T. Lu, K. Brezinsky, F.N. Egolfopoulos, D.F. Davidson, R.K. Hanson, C.T. Bowman, H. Wang, A physics-based approach to modeling real-fuel combustion chemistry - II. Reaction kinetic models of jet and rocket fuels, Combustion and Flame 193 (2018) 520-537.