Calculated Variation In Adiabatic Combustion Temperature For An Oxygen Reaction With Certain Elements As Reported By Grosse
| Atomic Number | Atomic Weight | Element | Temperature of Combustion deg R | Heating Number Value BTU/LB |
| 1 | ~1 | hydrogen | ~5,400 | ~52 |
| 2 | ~4 | helium | inert |
| 3 | ~7 | lithium | ~4,700 | ~18 |
| 4 | ~9 | beryllium | ~7,900 | ~28 |
| 5 | ~10 | boron | ~5,400 | ~26 |
| 6 | ~12 | carbon | ~3,700 | ~14 |
| 7 | ~14 | nitrogen | ~( 2,200) | quasi-inert with O |
| 8 | ~16 | oxygen | .......... | oxidizer |
| 9 | ~19 | fluorine | .......... | oxidizer |
| 10 | ~20 | neon | .......... | inert |
| 11 | ~23 | sodium | ~3,800 | ~4 |
| 12 | ~24 | magnesium | ~6,100 | ~11 |
| 13 | ~27 | aluminum | ~7,000 | ~13 |
| 14 | ~28 | silicium | ~4,600 | ~12 |
| 15 | ~31 | phosphorus | ~(2,400) | ~11 |
| 16 | ~32 | sulphur | ~(1,800) | ~4 |
| 17 | ~35 | chlorine | ~(400) | oxidizer |
| 18 | ~40 | argon | .......... | inert |
| 19 | ~39 | potassium | ~3,100 | ~2 |
| 20 | ~40 | calcium | ~6,900 | ~7 |
| 21 | ~45 | scandium | ~7,100 | ~8 |
| 22 | ~48 | titanium | ~6,000 | ~9 |
| 23 | ~51 | vanadium | ~6,000 | ~7 |
| 24 | ~52 | chromium | ~6,000 | ~6 |
| 25 | ~55 | manganese | ~6,200 | ~5 |
| 26 | ~56 | iron | ~5,500 | ~4 |
| 27 | ~59 | cobalt | ~(4,300) | ~3 |
| 28 | ~59 | nickel | ~(3,000) | ~2 |
| 29 | ~64 | copper | ~2,200 | ~1 |
| 30 | ~65 | zinc | ~4,000 | ~3 |
| 31 | ~70 | gallium | ~4,900 | ~3 |
| 32 | ~73 | germanium | ~5,600 | ~3 |
| 33 | ~75 | arsenic | ~(3,000) | ~3 |
| 34 | ~79 | selenium | ~(1,700) | ~3 |
| 35 | ~80 | bromine | ~(400) | oxidizer~2
| 36 | ~84 | krypton | ~....... | inert |
| 37 | ~85 | rubidium | ~2,900 | ~1 |
| 38 | ~88 | strontium | ~6,400 | ~2 |
| 39 | ~89 | yttrium | ~7,400 | ~3 |
| 40 | ~91 | zirconium | ~8,700 | ~4 |
| 41 | ~93 | niobium | ~7,300 | ~3 |
| 42 | ~96 | molybdenum | ~5,500 | ~2 |
| 43 | ~99 | technetium | ~........ | ~1 |
| 44 | ~101 | rubidium | ~........ | ~1 |
| 45 | ~103 | rhodium | ~........ | ~1 |
| 46 | ~106 | palladium | ~1,300. | .~1 |
| 47 | ~108 | silver | ~1,200 | ~1 |
| 48 | ~112 | cadmium | ~3,100 | ~1 |
| 49 | ~115 | indium | ~4,100 | ~1 |
| 50 | ~119 | tin | ~4,900 | ~2,5 |
| 51 | ~122 | antimony | ~3,100 | ~2 |
| 52 | ~128 | tellurium | .......... | ~2 |
| 53 | ~127 | iodine | .......... | ~1 |
| 54 | ~131 | xenon | .......... | inert |
| 55 | ~133 | cesium | ~2,700 | ~1 |
| 56 | ~137 | barium | ~5,400 | |
| 57 to 71 | | : | | rare earths |
| 72 | ~178 | hafnium | ~8,700 | |
| 73 | ~181 | tantalum | ~(7,600) | |
| 74 | ~184 | tungsten | ~5,800 | |
| 75 | ~186 | rhenium | ~(4,000) | |
| 76 | ~190 | osmium | ~(1,800) | |
| 77 | ~193 | iridium | ~(1,400) | |
| 78 | ~195 | platinum | ~800 | |
| 79 | ~197 | gold | ~600 | |
| 80 | ~201 | mercury | ~1,000 | |
| 81 | ~204 | thallium | ~(2,000) | |
| 82 | ~207 | lead | ~3,200 | |
| 83 | ~209 | bismuth | ~3,600 | |
| 84 | ~210 | polonium | ~(2,100) | |
| 85 | ~210 | astatine | ~(1,000) | |
| 86 | ~222 | radon | ......... | inert |
| 87 | ~223 | francium | ~2,400 | |
| 88 | ~226 | radium | ~4,500 | |
| 89 | ~227 | actinium | ~7,000 | |
| 90 | ~232 | thorium | ~9,000 | |
Some double-base propellant compositions:
J.P. powder:
Nitrocellulose(13.25%N2): 52.2%
Nitroglycerin: 43.0%
Diethyl phthalate: 3.0%
Diphenylamine: 0.6%
Potassium Nitrate(saltpeter): 1.1%
Nigrosine: 0.1%
J.P.N. powder:
Nitrocellulose(13.25%N2): 51.50%
Nitroglycerin: 43.00%
Diethyl phthalate: 3.00%
Ethyl centralite: 1.00%
Potassium sulfate: 1.25%
Carbon black: 0.20%
Candelilla wax: 0.05%
Slow burning powder:
Nitrocellulose(12.2%N2): 56.5%
Nitroglycerin: 28.5%
Dinitrotoluene: 11.0%
Ethyl centralite: 4.4%
Candelilla wax: 0.1%
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Relative value of Specific Impulse:
Black powder:-----------------------~125 sec.
Double-base:------------------------~200 sec.
Cellulose acetate+ammonium nitrate: ~175 sec.
Asphalt+ammonium perchlorate:-------~180 sec.
Polysulfide+ ":---------------------~200 sec.
Polyurethane+":---------------------~225-230 sec.
Polybutadiene+ ":-------------------~230-235 sec.
Polyurethane+ Aluminum + " :--------~240 sec.
Polybutadiene+ Aluminum + ":--------~245 sec.
PBAA + Aluminum + ":----------------~250 sec.
Composite/double-base:--------------~275 sec.
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List Of Ingredients Used In Double-Base Propellants
Plasticizer (Fuel And Oxidizer)
--NG: nitroglycerin
--TMETN: trimethylolethane trinitrate
--TEGDN: triethylene glycol dinitrate
--DEGDN: diethylene glycol dinitrate
Plasticizer (Fuel)
--DEP: diethylphtalate
--TA: triacetine
--PU: polyurethane
Binder (Fuel And Oxidizer)
--NC: nitrocellulose
Stabilizer
--EC: ethyl centralite
--2NDPA: 2-nitrodiphenilamine
Burning Rate Catalyst
--PbSa: lead salicylate
--PbSt: lead stearate
--Pb2EH: lead 2-ethylhexoate
--CuSa: copper salicylate
--CuSt: copper stearate
--LiF: lithium fluoride
High Energy Additive
--RDX: cyclotrimethylene trinitramine
--HMX: cyclotetramethylene tetranitramine
--NGD: nitroguanidine
Coolant
--OXM: oxamide
Opacifier
--C: carbon black
Flame Supressant
--KNO3: potassium nitrate (saltpeter)
--K2SO4: potassium sulfate
Metal Fuel
--Al: aluminum
Combustion Instability Suppressant
--Al: aluminum
--Zr: zirconium
--ZrC: zirconium carbide
List Of Ingredients Used For Composite Propellants
Oxidizer
--AP: ammonium perchlorate
--AN: ammonium nitrate
--NP: nitronium perchlorate
--KP: potassium perchlorate
--RDX: cyclotrimethylene trinitramine
--HMX: cyclotetramethylene tetranitramine
Binder
--PS: polysulfide
--PVC: polyvinyl chloride
--PU: polyurethane
--CTPB: carboxyl terminated polybutadiene
--HTPB: hydroxyl terminated polybutadiene
Curing And/Or Crosslinking Agents
--PQD: paraquinone dioxime
--TDI: toluene-2,4-diisocyanate
--MAPO: tris(1-(2-methyl) aziridinyl) phosphine oxide
--ERLA-O51O: N,N,O-tri (1,2-epoxy propyl)-4-aminophenol
--IPDI: isophorone diiosocyanate
Bonding Agent
--MAPO: tris( 1-(2-methyl) aziridinyl) phosphine oxide
--TEA: triethanolamine
--MT-4: adduct of 2.0 moles MAPO, 0.7 mole azipic acid,
.........and 0.3 mole tararic acid
Plasticizer
--DOA: dioctyl adipate
--IDP: isodecyl pelargonete
--DOP: dioctyl phthalate
Burning Rate Catalyst
--Fe2O3: ferric oxide
--FeO(OH): hydrated ferric oxide
--nBF: n-butyl ferrocene
--DnBF: di-n-butyl ferrocene
--LiF: lithium fluoride
Metal Fuel
--Al: aluminum
--Mg: magnesium
--Be: beryllium
--B: boron
Combustion Instability Suppressant
--Al: aluminum
--Zr: zirconium
--ZrC: zirconium carbide
THERMOPLASTIC BINDERS
Binder Oxidiser Agency Process
Plasticised 50/50 KNO2/Ammonium Monsanto Compression Picrate Formed
Ethyl Cellulose
Polyisobutylene British Compression Formed
Polyvinyl Acetate Ammonium Nitrate Still Limited Use
Polyvinyl Chloride Mix, cast, high temp
THERMOSET BINDERS
Polyester Ammonium Perchlorate Aerojet Cast, cure, cartridge load
Potassium Perchlorate (Aeroplex)
Polysulfide Ammonium Perchlorate JPL/Thiokol Cast in case /case bonded
Butadiene Ammonium Nitrate Phillips Petroleum Extruded-cartridge
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