NH3

Ammonia (NH3) was used as the fuel in the XLR-99 engine that powered the X-15 manned spaceplane; used as the propellant in some electric engine designs; developed as the propellant in Russian nuclear-powered ICBM designs of the 1950’s.

Reference Points

NH3 == Ammonia

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Tref Pref SG Cp dHvap Visc Cond Surf
SourceRpsiag/mlBTU/lbm-RBTU/lbmpoiseBTU/hr-ft-Rlbf/in
RocketProps431.714.70.68201.063589.22.555e-030.38492.555e-04
AFRPL-TR-69-149431.614.70.68191.065588.22.527e-030.32781.942e-04
RefProp431.714.70.68201.063589.22.555e-030.38492.555e-04
Aerojet431.614.70.68491.068596.22.453e-030.2171---

Fluid Properties

NH3 == Ammonia

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MolWt Tc Pc SGc Zc Tnbp Tmelt omega
Sourceg/gmoleRpsiag/ml(-)RR(-)
RocketProps17.030729.71643.70.22500.2545431.7351.90.25601
AFRPL-TR-69-14917.032730.11647.50.23500.2442431.6351.7---
Gas&Liq 5th Ed17.031729.71646.60.23500.2441431.7351.70.25700
RefProp17.030729.71643.70.22500.2545431.7351.90.25601
Aerojet17.032729.81636.00.24810.2298431.6351.80.23259

Vapor Pressure

_images/NH3_Psat.png


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Density

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Heat Capacity

_images/NH3_Cp.png


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Viscosity

_images/NH3_Visc.png


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Heat of Vaporization

_images/NH3_Hvap.png


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Thermal Conductivity

_images/NH3_Cond.png


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Surface Tension

_images/NH3_Surf.png


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