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. 2021 Apr 27;6(18):11813–11821. doi: 10.1021/acsomega.1c01115

Table 11. Performance and Sensitivity Values of Some Commonly Encountered Ingredients in Double- and Triple-Base Propellant Formulations.

data category NC NG NQ EGDN DEGDN TEGDN BTTN TMETN BuNENA DINA
Tma [°C]   14   –22 –10.9 –19 –27 –3 –9 51.3
Tdecb [°C] 192–209 150 248.9 175 160 170   182 180 177.5
ΩCO2c [%] –28.7 +3.5 –30.7 0 –40.8 –66.7 –16.6 –34.5 –104.3 –26.6
ΩCOd [%]   +24.7 –15.7 +21 –8.2 –26.7 –10.5 –3.14 –57.9 0
ρe [g cm–3] 1.67 1.591 1.71 1.48 1.38 1.335 1.52 1.46 1.22 1.488
Vdete [ms–1] 7300 7600 8200 7300 6600 2000   7050   7580
ΔfH°f [kJ mol–1] –1435.1 –370.1 –93 –244.8 –436.8 –629.9 –406 –425.2 –192.5 –448.2
ISh [J] 3 0.2 >49 0.2 0.2 12.7 1 9.2 6 6
FSi [N] >353 >353 >353 >353 >353 >353 >353 >353 >353 >353
a

Tm = onset temperature of melting.

b

Tdec = onset temperature of decomposition.

c

ΩCO2 = CO2 oxygen balance.

d

ΩCO = CO oxygen balance.

e

ρ = derived density from X-ray data.

f

Vdet = detonation velocity.

g

ΔfH° = molar enthalpy of formation.

h

IS = impact sensitivity.

i

FS = friction sensitivity.