Anhydrous Hydrazine (AH)
Monomethyl Hydrazine (MMH)
Uns- Dimethyl Hydrazine (UDMH)

Hydrogen Peroxide(H₂O₂)

Dinitrogen Tetroxide(N₂O₄)

Hydroxyl-Terminated Polybutadiene(HTPB)

Ammonium Perchlorate (AP)

Ethylamine

MSDS name:Hydrazine Anhydrous

CAS No:  302-01-2

Usage:  Used as a rocket propellant or an energy resource of
gas generator

Specification
Purity(AH), %                     98.5--99.0 min.
Water, %                                  1.5--1.0   max.
Particulate,  mg/l                         1      max.
Non-volatile residue, ppm       30      max.
Iron,                               ppm        5      max.
Chloride,                       ppm        5      max.
Carbon dioxide(CO2),   %           0.02 max.
Aniline                                          none
Appearance Colorless Transparent Even Liquid

Package: Stainless Steel Drum

MSDS name: Methylhydrazine

CAS No:  60-34-4

Usage: Used as a rocket propellant and raw material of herbicide
and pesticide

Specification
Purity(MMH), %        98.6 min.
Water, %                       1.2 max.
Particulate, mg/l        7    max

Package: Stainless Steel Drum

MSDS name:1,1-Dimethylhydrazine

CAS No: 57-14-7

Usage: Used as a rocket propellant, an additive and
a stabilizer, also used in plastics, rubbers, dyestuff industry

Specification
Appearance: colorless or light yellow transparent liquid
Purity(UDMH),        % (m/m)     98.0 min.
Water,                        % (m/m)       0.25 max.
Metahydrazone,       % (m/m)      1.35 max.
Dimethylamine,       % (m/m)      0.40 max.
Particulate,                     mg/l         10 max.

Package: ISO tank

CAS No：7722-84-1

Usage: Used as a rocket propellant

Specification

Hydrogen peroxide          90.0 --- 92.0%
Free acid (As H₂SO₄)          0.005% max.
Non-volatiles                       0.005% max.
Chloride (Cl- )                    0.0001% max.
Sulphate (SO₄^2-)                0.0003% max.
Nitride (N)                            0.001% max.
Phosphate (PO₄^3-)             0.0003% max.
Aluminum (Al)                0.00002% max.
Tin (Sn)                              0.00002% max.
Iron (Fe)                            0.00002% max.
Copper (Cu)                     0.00002% max.
Arsenic (As)                      0.00002% max.
Lead (Pb)                          0.00002% max.
Total organic carbon (TOC)    0.002% max.
Stability                             97% min.

CAS No：10544-72-6

Usage: Used as a rocket propellant

Specification

Purity(N₂O₄),  %                  99.5   min
Water,  %                                 0.15 max
Particulate, mg/L                10      max

Density at 15°C, g/cm³     1.458± 0.003

Package: ISO tank or drum
　

CAS No：69102-90-5

Usage: Used in all sort of motor with solid chemical propellant and space flight

Package: Polyethylene-lined Metal Drum

CAS No：7790-98-9

Usage: An important oxidizer used in solid rocket propellants

Specification

Purity(AP), %        99.5 min

Package: Drum

CAS No：75-04-7

Usage: Used to make organic chemicals including rubber vulcanization accelerators, pesticides, quaternary ammonium compounds, photographic chemicals,  corrosion inhibitors, explosives, dyes and pharmaceuticals.

Specification

Ethylamine,                             ≥99.5%
Ammonia                                   ≤0.1%
Diethyl amine:                          ≤0.2%
Triethyl amine:                         ≤0.05%
Alcohol:                                     ≤0.1%
Water:                                        ≤0.1%

Package: Steel Drum