High energy propellant

4533415
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Inventors

Wagner, III, Frederick B.
Izbicki, Anthony J.

Application #

836887

Filed

Sep-23-1977

Published

Aug-6-1985

Current US Class

149/35
149/92
149/93
264/3.1

International Classes

C06B 035/00

Field of Search

149/35 149/92 149/93 149/109.6

Assignee

Wagner, III; Frederick B. (Elmer, NJ)

US Patent References

3977924   Coolant additives fo...

Referenced by:

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Citation

Cite This Patent

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Abstract
A high energy propellant or explosive charge is prepared by compacting a normally pulverulent secondary high explosive, such as HMX or RDX, and retaining the pulverulent material packed as a coherent mass by means of a bridging agent capable of hydrogen bonding with the secondary explosive. The bridging agents used in this invention are characterized in their ability to hydrogen bond to the secondary explosive, their comparatively high intrinsic density, their solubility in a polar solvent, and their stereo compatibility with the secondary high explosive. The bridging agents are also characterized by the presence of at least two sites for hydrogen bonding comprised of hydroxyl or, carboxyl groups.
 
Claims
We claim:

1. A high energy propellant comprising a normally pulverulent secondary high explosive held together as a cohesive mass by means of a bridging agent which is a clathrate having a plurality of hydrogen-active sites.

2. A propellant according to claim 1 wherein the high explosive molecules have pendant nitro groups.

3. A propellant according to claim 2 wherein the high explosive is Beta-cyclotetramethylenetetranitramine or cyclotrimethylenetrinitramine.

4. A propellant according to claim 1 wherein the bridging agent has an intrinsic density greater than about 1.2.

5. A propellant according to claim 1 wherein the bridging agent is soluble in a polar solvent.



Description
BACKGROUND OF THE INVENTION

This invention relates to the preparation of propellants and explosive charges having high specific impulse and high detonation velocities. More particularly, it relates to the utilization of secondary high explosives such as Beta-HMX and RDX which are physically similar in that they exist only in pulverulent form and chemically similar in that they have pendant nitro groups as part of their molecular configuration. While it should be understood that this invention relates broadly to these types of secondary high explosives, the invention is discussed with particular reference to Beta-HMX (cyclotetramethylenetetranitramine) because of its high density and superior detonation velocity and pressure, although it is not intended that the invention should be so limited.

Beta-HMX is a known secondary high explosive having a high density, high specific impulse and high detonation velocity. While its relatively high cost, as compared, for example, to TNT, has limited the uses to which it has been applied, it has assumed considerable importance in the space program where the release of high bursts of energy are required. The need for such a propellant will become even greater as the space quest moves toward planets such as Venus and Jupiter which, due to their dense atmospheres that are several orders of magnitude greater than Earth's, require the development of substantial kinetic energy in order to effect course corrections, the powering of retro rockets, and the like.
 
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