Charge temperature is one of the main tactical and technical indices for a large caliber self-propelled gun, and is a critical firing datum affecting the projectile muzzle velocity and gun firing accuracy. In this paper, on the basis of analyzing the heat transfer character of propellant, an unsteady-state heat conduction model describing the variation of the charge temperature is built and the finite-difference implicit schemes are theoretically deduced using the volume equilibrium method for numerical simulation. Comparing simulation curves with experiment results indicates that the physical models used reflect the real-time change process of the charge temperature with the environment temperature. A noncontact automatic online charge temperature measurement unit is developed. This unit can accurately measure the temperature field and real-time average temperature of the charge for all charge zones placed in a combat vehicle and simultaneously transfer the temperature information to the gunner task terminal computer through a controller area network (CAN) bus interface for trajectory calculation and firing data correction, ensuring the weapon system meets the requirements of digitalization and informatization.

References

1.
Zhou
,
Y. H.
,
Yu
,
Y. G.
,
Liu
,
D. J.
, and
Lu
,
X.
,
2007
, “
Necessity of Precision Measuring of Charge Temperature in Field Environment
,”
J. Nanjing Univ. Sci. Technol.
,
31
(
5
), pp.
554
558
.
2.
Guo
,
X. F.
,
2004
,
Firing Accuracy Analysis for Long Range Gun Weapon Systems
,
National Defence Industry Press
,
Beijing
, pp.
80
81
.
3.
Tao
,
W. Q.
,
2001
,
Numerical Heat Transfer (Second Edition)
,
Xi'an Jiao Tong University Press
,
Xi'an, P. R. C.
, pp.
85
86
.
4.
Zhou
,
Y. H.
, and
Wang
,
S. C.
,
1990
,
Applied Two-Phase Flow Interior Ballistics
,
Ordnance Industry Press
,
Beijing
, pp.
78
79
.
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