Hydrazine: Difference between revisions
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Footgunning myself at this point |
Update data to 0.2.6203.27017 values(assuming the changes mentioned on changelog were the only ones) |
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| coefficient_b = 9.15642808045339 <!-- Chemistry.COEFFIENT_B_HYDRAZINE (sic) --> | | coefficient_b = 9.15642808045339 <!-- Chemistry.COEFFIENT_B_HYDRAZINE (sic) --> | ||
| thermal_efficiency = 0.08 <!-- Liquid hydrazine: 0.00 --> | | thermal_efficiency = 0.08 <!-- Liquid hydrazine: 0.00 --> | ||
| enthalpy = | | enthalpy = 306 kJ / mol <!-- Chemistry.ENTHALPY_HYDRAZINE --> | ||
| liquid_volume = 30 L/kmol <!--Chemistry.MOLAR_VOLUME_HYDRAZINE--> | | liquid_volume = 30 L/kmol <!--Chemistry.MOLAR_VOLUME_HYDRAZINE--> | ||
| molar_mass = 32 g/mol | | molar_mass = 32 g/mol | ||
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== Description == | == Description == | ||
<blockquote><q>Hydrazine is the perfect fuel for space exploration as it requires no oxidiser to combust, only needing heat or a spark. It is more commonly stored in its liquid form Liquid Hydrazine which is stable at room temperature. Hydrazine is extremely reactive and will violently combust in the presence of an oxidiser. It is extremely toxic to all forms of life.</q><br> | <blockquote><q>Hydrazine is the perfect fuel for space exploration as it requires no oxidiser to combust, only needing heat or a spark. It is more commonly stored in its liquid form Liquid Hydrazine which is stable at [[room]] temperature. Hydrazine is extremely reactive and will violently combust in the presence of an oxidiser. It is extremely toxic to all forms of life.</q><br> | ||
'''- Stationpedia'''</blockquote> | '''- [[Stationpedia]]'''</blockquote> | ||
'''Hydrazine''' or '''N<sub>2</sub>H<sub>4</sub>''' is a [[Hypergol]]. Hydrazine will spontaneously autoignite at 520.8 K (247.7°C), or at any temperature in the presence of [[Oxygen]], [[Ozone]] or [[Nitrous Oxide]].<!--untested--> | '''Hydrazine''' or '''N<sub>2</sub>H<sub>4</sub>''' is a [[Hypergol]]. Hydrazine will spontaneously autoignite at 520.8 K (247.7°C), or at any temperature in the presence of [[Oxygen]], [[Ozone]] or [[Nitrous Oxide]].<!--untested--> | ||
=== Combustion === | === Combustion === | ||
* 1 mol N2H4 -> 4 mol [[Pollutant|X]] + | * 1 mol N2H4 -> 4 mol [[Pollutant|X]] + 306 kJ (autoignition at 247.7°C) | ||
== Usage == | == Usage == | ||
''See also: [[Fuel]]'' | ''See also: [[Fuel]]'' | ||
Hydrazine has a low combustion enthalpy, making it suboptimal for rocketry applications that require high performance. However, the fact it is a monopropellant allows its use in a [[Pumped Gas Engine]] or [[Pressure-Fed Liquid Engine]] without requiring any premixing, simplifying rocket and/or launch pad design. | Hydrazine has a low combustion enthalpy, making it suboptimal for [[rocketry]] applications that require high performance. However, the fact it is a monopropellant allows its use in a [[Pumped Gas Engine]] or [[Pressure-Fed Liquid Engine]] without requiring any premixing, simplifying rocket and/or launch pad design. | ||
===Notes=== | ===Notes=== | ||
Revision as of 02:02, 13 March 2026
| Gas icon | |
| Phase Change Information | |
|---|---|
| Specific Heat | 48.4 J/mol*K |
| Latent Heat | 4000 J/mol |
| Min Condensation Pressure | 6.3 kPa at 246.236749353 K |
| Max Liquid Temperature | 6000 kPa at 520.807708414 K |
| Freezes at | 246.236749353 K |
| Liquid Volume | 30 L/kmol |
| Molar Mass | 32 g/mol |
Description
Hydrazine is the perfect fuel for space exploration as it requires no oxidiser to combust, only needing heat or a spark. It is more commonly stored in its liquid form Liquid Hydrazine which is stable at room temperature. Hydrazine is extremely reactive and will violently combust in the presence of an oxidiser. It is extremely toxic to all forms of life.
- Stationpedia
Hydrazine or N2H4 is a Hypergol. Hydrazine will spontaneously autoignite at 520.8 K (247.7°C), or at any temperature in the presence of Oxygen, Ozone or Nitrous Oxide.
Combustion
- 1 mol N2H4 -> 4 mol X + 306 kJ (autoignition at 247.7°C)
Usage
See also: Fuel
Hydrazine has a low combustion enthalpy, making it suboptimal for rocketry applications that require high performance. However, the fact it is a monopropellant allows its use in a Pumped Gas Engine or Pressure-Fed Liquid Engine without requiring any premixing, simplifying rocket and/or launch pad design.
Notes
TBW
Sources
| Source | Amount |
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| ? | ? |
References
Gases and Liquids
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