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Sam Moy Phones & Addresses

  • 69 Glassboro Rd, Parsippany, NJ 07054 (973) 884-9274
  • Oakland Gardens, NY
  • Guilderland, NY

Business Records

Name / Title
Company / Classification
Phones & Addresses
Sam Moy
President
Fong's Laundry Inc
Drycleaning Plant Power Laundry · Dry Cleaning
36 Elm Pl, Rye, NY 10580
(914) 967-4036
Sam Moy
Principal
Moy Sam Corp
Business Services, Nec, Nsk
3807 Main St, New York, NY 10003
Sam Moy
Vice-President
Valueoptions, Inc
Individual/Family Services · Managed Health Care Programs
433 Riv St, Troy, NY 12180
(518) 270-1806, (518) 270-4722, (518) 271-2804

Publications

Wikipedia

The Chris Moyles Show

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Matt Fincham: Assistant Producer of the show. Freya Mehta: Day Producer since Monday 13 June 2011, replacing previous day producer Sam Moy who left for 6 ...

Us Patents

High Energy Thermoplastic Elastomer Propellant

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US Patent:
6997996, Feb 14, 2006
Filed:
Sep 12, 2000
Appl. No.:
09/665190
Inventors:
Thelma G. Manning - Montville NJ, US
Joseph L. Prezelski - Jermyn PA, US
Sam Moy - Parsippany NJ, US
Bernard Strauss - Rockaway NJ, US
James A. Hartwell - Elton MD, US
Arpad Juhasz - Joppatowne MD, US
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
C06B 45/10
C06B 25/34
D03D 23/00
US Classification:
149 196, 149 92, 1491096, 264 31
Abstract:
A high energy propellant, comprising an oxetane thermoplastic elastomer energetic binder admixed with a high energy explosive filler. The oxetane thermoplastic elastomer energetic binder preferably comprises from about five percent to about thirty percent by weight and the high energy explosive filler comprises from about seventy percent to about ninety-five percent by weight of the composition. A preferred propellant further includes an explosive plasticizer, preferably in an amount of about four percent to about seven percent of the plasticizer by weight of the propellant. The preferred filler is selected from the group consisting of CL-20, TNAZ, RDX and mixtures thereof. The preferred plasticizer is selected from the group consisting of TNAZ, BTTN, TMETN, TEGDN, BDNPA/F, methyl NENA, ethyl NENA and mixtures thereof. In a preferred embodiment, the propellant is actually a pair of high energy propellants comprising a mixture of first and second high energy propellants with the first propellant having a burning rate at least two times faster than the burning rate of the second propellant. The first propellant includes an oxetane thermoplastic elastomer energetic binder admixed with CL-20 high energy explosive filler.

Cross-Sectional Functionally Graded Propellants And Method Of Manufacture

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US Patent:
7896989, Mar 1, 2011
Filed:
Feb 11, 2005
Appl. No.:
10/906274
Inventors:
David Fair - Parsippany NJ, US
Dilhan M. Kalyon - Teaneck NJ, US
Sam Moy - Parsippany NJ, US
Leon R. Manole - Great Meadows NJ, US
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
C06B 45/00
C06B 45/04
C06B 45/06
D03D 23/00
D03D 43/00
US Classification:
1491096, 149 2, 149 17, 149 18, 1491094
Abstract:
Methods of making cross sectional, functionally-graded munitions propellants exhibiting various distributions of particle concentrations and burn rate, including having a fast burning core and slower burning outer layer(s). Unlike prior art methods of preparing such munitions, propellants prepared according to our inventive method(s) may be performed substantially as a single extrusion step or as a few processing steps, without requiring the time, expense and/or difficulties that characterized familiar, laminating methods and methods which use multiple extruders. Our inventive method advantageously employs a demixing phenomenon that, prior to our inventive application and teaching, has been considered quite undesirable in the preparation of propellants where uniformity and well-mixedness have been propellant attributes widely sought after.

High Energy Tnaz, Nitrocellulose Gun Propellant

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US Patent:
57984816, Aug 25, 1998
Filed:
Nov 7, 1996
Appl. No.:
8/743782
Inventors:
Thelma Manning - Montville NJ
Bernard Strauss - Rockaway NJ
Joseph P. Prezelski - Budd Lake NJ
Sam Moy - Parsippany NJ
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
C06B 4510
US Classification:
149 198
Abstract:
A high energy propellant, comprising at least one oxidizer; a nitrocellul binder; an ethyl centralite stabilizer; a plasticizer; and an oxetane thermoplastic elastomer energetic binder. The oxetane thermoplastic elastomer energetic binder comprises from about zero percent to about fifteen percent by weight of the propellant. The preferred oxidizer is selected from the group consisting of CL-20, TNAZ, RDX, HMX and mixtures thereof. The oxidizer comprises from about five percent to about forth percent by weight of the propellant. The nitrocellulose binder comprises from about fifteen percent to about fifty percent by weight of the propellant and the ethyl centralite stabilizer comprises from about 0. 7 percent to about 1. 5 percent by weight of the propellant.

Method Of Making High Energy Explosives And Propellants

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US Patent:
57165572, Feb 10, 1998
Filed:
Nov 7, 1996
Appl. No.:
8/744390
Inventors:
Bernard Strauss - Rockaway NJ
Thelma Manning - Montville NJ
Joseph P. Prezelski - Budd Lake NJ
Sam Moy - Parsippany NJ
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
C06B 2100
US Classification:
264 33
Abstract:
A method of formulating high energy explosives and propellants, including e steps of melting the explosive at a temperature just above its melting temperature, admixing and dissolving or plasticizing a binder, and extruding or casting the resultant solution into a useful form for further forming the resulting material into a munitions. The first step in this method includes the use of any high energy explosive material. Examples of these include hexanitrohexaazaisowurtzitane or CL-20, 1,3,3-trinitroazetidine or TNAZ, 2,4,6-trinitrotoluene or S-TNT, 1,3,5-trinitrobenzene or S-TNB, HMX, RDX, butane-trio-trinitrate or BTTN, trimethylolethane trinitrate or TMETN; triethylene glycol dinitrate or TEGDN, bis, 2,2-dinitro propyl acetal/bis 2,2 dinitro propyl formal or BDNPA/F, methyl nitrato ethyl nitramine or methyl NENA, ethyl NENA, mixtures thereof and the like. Binders that are useful for the present invention include cellulose acetate butyrate, ethyl centralite, oxetane thermoplastic elastomers, nitrocellulose, HYTREL and ESTANE polymers, and the like.

Insensitive High Energy Explosive Compositions

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US Patent:
48426598, Jun 27, 1989
Filed:
Apr 22, 1988
Appl. No.:
7/184930
Inventors:
Mark Mezger - Hackettstown NJ
Bernard Strauss - Rockaway NJ
Sam M. Moy - Parsippany NJ
Joseph L. Prezelski - Budd Lake NJ
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
C06B 4510
US Classification:
149 192
Abstract:
A high energy explosive composition containing 80 to 95 percent HMX having low susceptibility to sympathetic detonation. The composition also contains between 2. 9 to 10 percent cellulose acetate butyrate, 10 to 17. 1 percent of 1:1 mixture of bis 2,2-dinitropropyl acetate and bis 2,2-dinitropropyl formal, and 0. 5 percent tri (dioctyl phosphato) titanate.

Multi-Layer High Energy Propellants

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US Patent:
56908687, Nov 25, 1997
Filed:
Nov 7, 1996
Appl. No.:
8/744392
Inventors:
Bernard Strauss - Rockaway NJ
Thelma Manning - Montville NJ
Joseph P. Prezelski - Budd Lake NJ
Sam Moy - Parsippany NJ
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
C06B 2100
C06B 4510
US Classification:
264 31
Abstract:
A multi-layer propellant and a method for making the same is provided, in ich the propellant has at least one slow burning formulation and at least one fast burning formulation, such that the ratio of these burning rates is at least 2:1. The propellant produces an impetus of at least 1300 Joules/gm. The preferred binder is a high energy oxetane thermoplastic elastomer. The preferred slow burning formulation employs RDX, while the preferred fast burning formulation employs CL-20. The two formulations are formed separately, such as in layers that are then fused, using the bonding strength of the binder. The shape may be any shape that is useful in munitions and may include one or many layers of each burning rate. Preferred shapes include a multi-layered propellant with one slow burning formulation on top and a bottom layer of the fast burning formulation. The layers may be formed from ribbons, discs, cones, truncated cones and partial spheres.

Insensitive Gun Propellant

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US Patent:
53257820, Jul 5, 1994
Filed:
Jul 20, 1993
Appl. No.:
8/093914
Inventors:
Bernard Strauss - Rockaway NJ
Sam M. Moy - Parsippany NJ
Assignee:
The United States of America as represented by the Secretary of the Army - Washington DC
International Classification:
C06B 4512
US Classification:
102285
Abstract:
A gun propellant having reduced sensitivity to impact and improved burning ate, comprising crystallized NNHT particles admixed with a binder and at least one plasticizer. In a preferred embodiment, the binder is a nitrocellulose binder and the plasticizer is a liquid nitramine plasticizer. A preferred liquid nitramine plasticizer is selected from the group of ethyl nitrato ethyl nitramine and methyl nitrato ethyl nitramine. The propellant of this invention may be used or alone or may also include a quantity of RDX propellant. The propellant is suitable to be formulated for an artillery application or for a tank system.
Sam Ming Moy from Parsippany, NJ, age ~70 Get Report