Inventor

SAYLES DAVID C

US77 patents

⚠️ This page may combine multiple inventors who share the name “SAYLES DAVID C”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

SAYLES DAVID C

US ARMY

Fire protective blanket

Method of safely detoxifying mustard gases

Method of making edible coatings for protecting perishable foods against spoilage

Extinguishing rocket/missile solid propellants

Signal or rescue flare of variable luminosity

Disposal of solid propellants

Ultrafast, linearly-deflagration ignition system

Method of manufacturing hybrid fiber-reinforced composite nozzle material

Thermoplastic para-polyphenylene sulfide, high temperature-resistant rocket motor cases

Microcoacervation of propellant ingredients

Method of preparing non-composite, thermoplastic, high-temperature-resistant rocket motor cases

Apparatus for testing candidate rocket nozzle materials

Method of chemical bonding of solid propellant grains to the internal insulation of an interceptor motor

Hypervelocity penetrator for an electromagnetic accelerator

Mechanical enhancement of the burning rate of solid propellants by means of shrink tubes or spheres

Ultra-ultrahigh burning rate composite modified double-base propellants containing porous ammonium perchlorate

High intensity yellow smoke and flame flare compositions

Method of increasing the burning rate enhancement by mechanical accelerators

Impermeable liner-barrier for propellants containing a high content of carborane burning rate accelerator

Non nitroglycerin-containing composite-modified double-base propellant

A processing method for increasing propellant burning rate

Burning rate enhancement of solid propellants by means of metal/oxidant agglomerates

Sabot for an electromagnetically-accelerated, unguided hypervelocity penetrator

Cure shrink-resistant missile motor cases

Microwave drying of ammonium perchlorate grinding spheres

Method of generating single-event, unconfined fuel-air detonation

Increasing burning rate of solid propellants by electric field effects

Thermolysis of tetraalkylammonium borohydrides to bis(tetraalkylammonium) decahydrodecaboranes

Method of imparting hypergolicity to non-hypergolic rocket propellants

Liner-barrier for ultrahigh burning rate propellants

Conductance method for determining the mechanical properties of propellants

Method for preparation of a carboranyl burning rate accelerator precursor

Reignition suppressants for solid extinguishable propellants for use in controllable motors

Nuclear blast-resistant rocket motor cases

High nitrogen content gas generant and method of producing near-neutral combustion products

Ultrahigh burning rate propellants containing an organic perchlorate oxidizer

Anti-erosive, solid rocket propellant compositions

Solid propellant with iron-carbonyl containing polymer binder

Pressure exponent suppressants

Composite thermoplastic filler for ballast cans for use with fluorescent lights

Cloth-lined interceptor motor insulation for strong insulation-to-propellant interlock

Composite rocket propellant composition with a controllable pressure exponent

Heat-expandable beads as burning rate accelerators

Structurally-strong solid propellants

Method of ejecting an interceptor missile from its silo

Encapsulated signal illumination flare composition

Embedded explosives as burning rate accelerators for solid propellants

SAYLES DAVID C

Siloxane-based elastomeric interceptor motor insulation

Non-shrinking, dimensionally-stable modified epoxy resins

USA

Method of controlling the increase in potlife of propellants during processing