2-Hydroxymethyl-1,3-propanediol preparation

4336408
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Inventors

Barnes, Michael W.

Application #

052155

Filed

Jun-26-1979

Published

Jun-22-1982

Current US Class

149/47
149/76
149/88
149/92
549/372
549/374
558/484
558/486
568/853

International Classes

C07C 031/22; C07C 029/14

Field of Search

568/853 568/862

Assignee

Thiokol Corporation (Newtown, PA)

Examiners

Evans; Joseph E.

Attorney, Agent or Firm

White; Gerald K.

US Patent References

4006190   Production of hydr...
4091040   Procedure for maki...

Referenced by:

View Backward References

Other References

Vik, "Acta Chimica Scandinavica", vol. 27 (1973), pp. 239-250. Boros et al., "J. A. C. S.", vol. 88 (1966), pp. 1140-1143.

Citation

Cite This Patent

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Abstract
2-Hydroxymethyl-1,3-propanediol trinitrate, processes for its preparation, and compounds related thereto are disclosed. The final product is useful as a plasticizer of relatively low volatility in double based propellant compositions and as a liquid explosive.
 
Claims
The subject matter which applicant regards as his invention is particularly pointed out and destinctively claimed as follows:

1. A process for the preparation of 2-hydroxymethyl-1, 3-propanediol which comprises the treatment of bis-(hydroxymethyl) acetaldehyde with an aldehyde carbonyl group reducing agent selected from hydrogen adsorbed on a hydrogenation catalyst or an alkali metal dissolving in a lower alkanol.

2. A process for the preparation of 2-hydroxymethyl-1,3-propanediol which comprises the treatment of bis-(hydroxymethyl)acetaldehyde with an aldehyde carbonyl group reducing agent selected from hydrogen adsorbed on a platinum, rhodium or palladium hydrogenation catalyst, or an alkali metal dissolving in a lower alkanol.



Description
BACKGROUND OF THE INVENTION

Double base and crosslinked double base propellants are well-known as high energy propellants. These propellants employ nitroglycerin as a plasticizer.

Nitroglycerin has a number of undesirable qualities which limits the usefulness of propellants employing it. The principal deficiencies are:

(1) Marginal thermal stability coupled with auto catalysis of the decomposition by the decomposition products requiring elaborate stabilization systems to provide adequate shelf life;

(2) Difficulty in achieving high solids loading;

(3) Difficulty in achieving good mechanical properties by using HMX coating agents; and

(4) A relatively high vapor pressure causing exudation during vacuum processing, and migration over long periods at ambient temperatures and pressures.

The present invention relates to a novel compound 2-hydroxymethyl-1,3-propanediol trinitrate and its use in replacing nitroglycerin in double base propellants to ameliorate the problems associated with the use of nitroglycerin.
 
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