Formula  Molecular wt 

[C_{6}H_{10}O_{n}]_{n}  114.14 
Coefficients for the Regression Equation
rdot = a G_{ox}^{n} rdot (in/sec) G_{ox} (lbm/sqinsec) 

p.s. sorry i don't currently recall the sources, only the data, if requested, I will find them. hg  
Coefficient  Source 1  Source 2  Source 3 

a  0.0440  0.0412  0.0608 
n  0.60  0.70  0.61 




Property  Symbol  Hung  Karabeyoglu  Wooldridge  Units 
Molecular Weight  MW  100.0      g/gmol 
Specific Heat (gas)  C_{P}  0.35
0.35 
0.37
 

 
cal/gK
Btu/lb_{m}R 
Specific Heat (solid)  C_{P}  0.31
0.31 

 

 
cal/gK
Btu/gK 
Heat of Formation  h^{o}  928
1670 

 

 
cal/g
Btu/lb_{m} 
Latent Heat of Gasification  L_{V}  130
234 
231
 
350
 
cal/g
Btu/lb_{m} 
Latent Heat of Fustion  L_{F}  85
155 

 

 
cal/g
Btu/lb_{m} 
Boiling Point  B.P.  374
673.2 

 

 
K
R 
Density  rho_{S}  1.683
150 
1.1
 

 
g/cm^{3}
lbm/ft^{3} 
Thermal Diffusivity  kappa    0.11    mm^{2}/sec 
Thermal Conductivity  k_{S}  0.0012
0.289 

 

 
cal/seccmK
Btu/hrftR 
Hung, et. al., "Further Analytical Study of Hybrid Rocket Combustion", NASI10210, 1972.
Karabeyoglu, et. al., "Transient Combustion in Hybrid Rockets," AIAA 952691, 1995.
Wooldridge, et. at., "Internal Ballistic Considerations in Hybrid Rocket Design," J. Spacecraft, Feb. 1967.