← ALL PROPELLANTS
HYPERGOLIC FUEL

Hydrazine (N2H4)

N₂H₄
Fuel (or Monopropellant)Storable at room temperature for yearsExtremely toxic — carcinogenic, corrosive, causes organ damage
N₂H₄
FORMULA
CHEMICAL
220–240 s (monopropellant), 280–310 s (bipropellant with NTO)
SECONDS
ISP RANGE
1.004 g/cm³ at 25°C
KG/M³
DENSITY
114°C
°C
BOILING POINT
32.05 g/mol
G/MOL
MOLECULAR WEIGHT
Extremely toxic — carcinogenic, corrosive, causes organ damage
RATING
TOXICITY

Hydrazine (N2H4) (N₂H₄) is a hypergolic fuel propellant used as a fuel (or monopropellant). Storable at room temperature for years. Typical ISP: 220–240 s (monopropellant), 280–310 s (bipropellant with NTO) seconds.

Hydrazine is a highly reactive, toxic, storable liquid propellant used extensively in spacecraft attitude control and orbital maneuvering systems. It can be used as a monopropellant (decomposed over a catalyst) or as a bipropellant fuel with an oxidizer. Despite its extreme toxicity, hydrazine’s reliability, storability, and consistent performance have made it indispensable in space operations for decades.

FormulaN₂H₄
🔬TypeHypergolic Fuel
🔥RoleFuel (or Monopropellant)
Density1.004 g/cm³ at 25°C kg/m³
Molecular Weight32.05 g/mol g/mol
🌡Boiling Point114°C°C
Melting Point1.4°C°C
🎨Color / AppearanceColorless oily liquid
📦StorabilityStorable at room temperature for years
CryogenicNo

Used since the 1950s in military and space applications. Remains the dominant monopropellant despite decades of effort to find safer alternatives.

Storable, hypergolic ignition (no igniter needed), reliable, high-density impulse

Extremely toxic, carcinogenic, requires SCAPE suits for handling, expensive safety measures

🚀ISP Range220–240 s (monopropellant), 280–310 s (bipropellant with NTO) seconds
ToxicityExtremely toxic — carcinogenic, corrosive, causes organ damage
CryogenicNo
Nitrogen Tetroxide (NTO)
MON (Mixed Oxides of Nitrogen)
Draco (SpaceX)
R-4D (Aerojet)
Various attitude control thrusters

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