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  • 07:3807:38, 20 April 2017 diff hist +3 Rocket propellant"usually at a temperature of 3000°C and a pressure of 300 kg/cm^2" -> "usually at very high pressures, with combustion temperatures approaching 3000K". kg/cm^2 not a valid unit of pressure, K is std unit for Temp., values are variable, no cite given

5 January 2017

  • 14:0714:07, 5 January 2017 diff hist −2 IUCLIDNo edit summary

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