Page 1 of 4

European Journal of Applied Sciences – Vol. 10, No. 2

Publication Date: April 25, 2022

DOI:10.14738/aivp.102.12039. Partom, Y. (2022). Initiation of an Explosive Charge by Consecutive Projectiles. European Journal of Applied Sciences, 10(2). 124-

127.

Services for Science and Education – United Kingdom

Initiation of an Explosive Charge by Consecutive Projectiles

Yehuda Partom

Retired from RAFAEL, P.O. Box 2250, Haifa, Israel

ABSTRACT

Test results reported in [1,2] show that when two consecutive projectiles hit an

explosive charge, and when their velocity is such that the first projectile is just

below the initiation threshold, the second projectile is able to initiate the explosive.

We propose here an explanation to this important phenomenon. Our explanation is

based on our reactive flow model TDRR for which the explosive reaction rate

increases with the reactant temperature. We use our reactive flow code to

demonstrate how this works. To simplify the computations, we hit the explosive

charge with two consecutive pressure pulses instead of with two projectiles.

INTRODUCTION

In [1.2] they report on a series of tests in which an explosive charge is initiated by two identical

consecutive projectiles. The tests show clearly that the explosive charge is initiated much more

easily by two consecutive projectiles than by a single identical projectile. In those tests the

impact by a single projectile is a little under the initiation threshold, but the impact of a second

identical projectile is able to cross the initiation threshold and lead to detonation.

In [1,2] they try to explain their test results by hand waving arguments. They assume (without

proof) that the first projectile deforms and damages the explosive on its path in a way that

makes it more sensitive to an additional impact. But it’s not possible to prove or disprove such

an explanation by computer modeling or other means.

The phenomenon reported in [1,2], that when a projectile hits an explosive charge below its

initiation threshold, it makes it more sensitive to the impact of an additional projectile, is of

practical importance when dealing with the response of explosives to impact by projectiles or

fragments. We therefore need to understand this phenomenon thoroughly, and be able to

predict it in detail by computer modeling. It seems to us that the explanation given in [1,2] is

not the correct one, and in what follows we propose an alternative explanation which we

demonstrate through computer simulations. The essence of our explanation is: 1) when a

projectile hits an explosive charge, or alternatively, when a pressure pulse acts on an explosive

charge, the explosive heats up to some residual temperature which increases with the strength

of the impact; 2) an additional projectile or pressure pulse hitting the same explosive charge

would heat it up some more and to a higher temperature; 3) as the reaction rate of an impacted

explosive increases with its reactant temperature (according to our reactive flow model called

TDRR [3-5], which we use later to demonstrate our claim), the explosive charge becomes more

sensitive to the consecutive impact.

In what follows we use our reactive flow model TDRR to demonstrate our explanation of the

test results reported in [1,2].

Page 2 of 4

125

Partom, Y. (2022). Initiation of an Explosive Charge by Consecutive Projectiles. European Journal of Applied Sciences, 10(2). 124-127.

URL: http://dx.doi.org/10.14738/aivp.102.12039

DOUBLE IMPACT SIMULATIONS WITH TDRR

To make our computer simulations simple we hit the explosive charge with boundary pressure

pulses instead of with projectiles. The application of pressure pulses is much simpler than that

of projectiles as there is no need to describe the projectiles and to follow their penetration path

and change of shape. Also, instead of looking for the initiation threshold of a single pulse and

then decreasing its strength somewhat, we compute and make comparisons of the run distance

to detonation of the assumed pressure pulses. We then check whether and by how much the

run distance from two consecutive pulses is lower than the run distance from a single pulse.

COMPUTATIONS

We use simple oblong pressure pulses of 10GPa strength and 1μs duration. We’re changing the

time difference between pulses between zero and a few microseconds. When the pulses are

without a time difference between them, we get:

• From a single pulse (1μs duration), the run distance is larger than 78mm (our charge

length).

• From 2 adjacent pulses the run distance is 21.30mm.

• From 3 adjacent pulses: 18.08mm.

• From 4 adjacent pulses: 18.08mm (no change).

• From 2 pulses 1 μs apart, the run distance goes down to 8.15mm.

• From 2 pulses 2μs or 3μs apart, the run distance stays the same, 8.15mm.

From these results we see clearly that by introducing a time difference between the two pulses,

the run distance to detonation decreases substantially, which means that the first pulse

increases the sensitivity (or the reaction rate) considerably.

As stated above, the main feature of the reactive flow model that we’re using is that the reaction

rate is an increasing function of the reactant temperature. Our computation results therefore

support our suggested explanation of the test results in [1,2]. Again, our explanation is that the

first pulse heats up the explosive without reacting it. Therefore, as reaction rate increases with

temperature of the reactant, the reaction rate from the second pulse is higher.

To demonstrate the higher temperature increase caused by two separate pulses compared to

the lower temperature increase caused by connected pulses, we show in Fig. 1 temperature

histories from two such computations.

Page 3 of 4

126

European Journal of Applied Sciences (EJAS) Vol. 10, Issue 2, April-2022

Services for Science and Education – United Kingdom

Figure 1. Reactant temperature histories at 4mm into the explosive charge.

Red: two connected pulses.

Blue: two pulses with 1μs time separation.

From Fig. 1 we see that the 10GPa pulse increases the reactant temperature by 500K (to 800K).

Then as a result of the rarefaction, the reactant temperature decreases back to 500K. When the

second pulse arrives, it increases the reactant temperature by 600K (to 1100K), because the

reactant temperature is now higher than before. But at such a temperature the reaction rate is

already substantial, and the reactant temperature increases even more up to 1150K. The end

result is that the run distance to detonation decreases substantially.

SUMMARY

Tests reported in [1,2] show that when two consecutive projectiles hit an explosive charge, they

are able to initiate it even when a single such projectile does not. In [1,2] they propose a hand

waving explanation to this important phenomenon, but they’re not able to provide proof to

their explanation.

We propose here our own explanation to the phenomenon observed in [1,2], that the explosive

sensitivity to the second projectile (or second pressure pulse) is higher than its sensitivity to

the first projectile (or pressure pulse). Our explanation is that the increased sensitivity results

from an increase of temperature of the explosive caused by the first pulse. This follows from

our reactive flow model TDRR [3-5] for which the reaction rate is an increasing function of the

reactant temperature.

We demonstrate how this comes about through our computer modeling code, which is based

on our reactive flow model TDRR.

Page 4 of 4

127

Partom, Y. (2022). Initiation of an Explosive Charge by Consecutive Projectiles. European Journal of Applied Sciences, 10(2). 124-127.

URL: http://dx.doi.org/10.14738/aivp.102.12039

References

[1]. P.J. Haskins et al., Dual fragment impact of PBX charges, SCCM (2017).

[2]. P.J. Haskins et al., Dual fragment impact, 15th Det. Symp., 657-664 (2014).

[3]. Y. Partom, Hydro-reactive computations with a temperature dependent reaction rate, SCCM conference, AIP 0-

7354-0068, 460-463 (2001).

[4]. Y. Partom, Characteristic code for shock initiation, LANL Report, LA-10773 (1986).

[5]. Y. Partom, A void collapse model for shock initiation, 7th Symp on detonation, 506 (1981).