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STORABLE OXIDIZER / MONOPROPELLANT

Hydrogen Peroxide (HTP)

H₂O₂
Oxidizer (or Monopropellant)Storable but slowly decomposes; requires passivated containersModerate — causes severe burns, strong oxidizer
H₂O₂
FORMULA
CHEMICAL
150–170 s (monopropellant), 250–300 s (bipropellant with kerosene)
SECONDS
ISP RANGE
1.45 g/cm³ (98% concentration)
KG/M³
DENSITY
150.2°C (decomposes before boiling at high concentrations)
°C
BOILING POINT
34.01 g/mol
G/MOL
MOLECULAR WEIGHT
Moderate — causes severe burns, strong oxidizer
RATING
TOXICITY

Hydrogen Peroxide (HTP) (H₂O₂) is a storable oxidizer / monopropellant propellant used as a oxidizer (or monopropellant). Storable but slowly decomposes; requires passivated containers. Typical ISP: 150–170 s (monopropellant), 250–300 s (bipropellant with kerosene) seconds.

High-test peroxide (HTP) is a concentrated form of hydrogen peroxide (85-98%) used as a monopropellant or oxidizer in rocket engines. When passed over a silver or platinum catalyst, it decomposes exothermically into steam and oxygen. HTP was used in early rocket programs including the V-2 turbopump drive, Mercury capsule attitude control, and the Black Arrow launch vehicle.

FormulaH₂O₂
🔬TypeStorable Oxidizer / Monopropellant
🔥RoleOxidizer (or Monopropellant)
Density1.45 g/cm³ (98% concentration) kg/m³
Molecular Weight34.01 g/mol g/mol
🌡Boiling Point150.2°C (decomposes before boiling at high concentrations)°C
Melting Point-0.43°C°C
🎨Color / AppearanceColorless (very pale blue at high concentrations)
📦StorabilityStorable but slowly decomposes; requires passivated containers
CryogenicNo

Used in the V-2 Walter turbine, Black Arrow, Mercury spacecraft, and early British rockets. Seeing renewed interest for green propulsion.

Storable, non-toxic exhaust, can serve as monopropellant, catalytic decomposition

Moderate Isp, slow decomposition in storage, material compatibility issues, can detonate

🚀ISP Range150–170 s (monopropellant), 250–300 s (bipropellant with kerosene) seconds
ToxicityModerate — causes severe burns, strong oxidizer
CryogenicNo
Kerosene
Ethanol
Catalyst (as monopropellant)
Gamma (Black Arrow)
Walter HWK 109-509 (Me 163)
Various satellite thrusters

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