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  2. Oxygenated treatment - Wikipedia

    en.wikipedia.org/wiki/Oxygenated_treatment

    Less flow resistance, lower dissolved feedwater iron concentrations, FeOOH film is more stable, reduced boiler cleaning frequency - Disadvantages: Increased risk of FAC, a deaerator is required, more frequent chemical cleaning is required, hazardous chemicals (hydrazine) are used. A deaerator is required. Air leakage is more serious.

  3. Bulk loaded liquid propellants - Wikipedia

    en.wikipedia.org/wiki/Bulk_loaded_liquid_propellants

    In the 1950s through 1970s, a mixture of 63% hydrazine, 32% hydrazine nitrate and 5% water was used in experimental 37mm gun firings and later in 120mm gun firings. The 32% hydrazine nitrate mixture was selected by extensive experiments to have a notably flat pressure profile, increasing gun safety.

  4. Hydrazine - Wikipedia

    en.wikipedia.org/wiki/Hydrazine

    Since hydrazine is a solid below 2 °C, it is not suitable as a general purpose rocket propellant for military applications. Other variants of hydrazine that are used as rocket fuel are monomethylhydrazine , CH 3 NHNH 2 , also known as MMH (melting point −52 °C), and unsymmetrical dimethylhydrazine , (CH 3 ) 2 NNH 2 , also known as UDMH ...

  5. Cost estimates come back for boiler, systems ... - AOL

    www.aol.com/cost-estimates-come-back-boiler...

    Nov. 21—The replacement of mechanical systems at three schools in the district is estimated to cost about $3.96 million, engineers with ISG Inc. presented to the Albert Lea school board Monday.

  6. Unsymmetrical dimethylhydrazine - Wikipedia

    en.wikipedia.org/.../Unsymmetrical_dimethylhydrazine

    UDMH is a derivative of hydrazine and is sometimes referred to as a hydrazine. As a fuel, it is described in specification MIL-PRF-25604 in the United States. [13] UDMH is stable and can be kept loaded in rocket fuel systems for long periods, which makes it appealing for use in many liquid rocket engines, despite its cost.

  7. Green Propellant Infusion Mission - Wikipedia

    en.wikipedia.org/wiki/Green_Propellant_Infusion...

    The propellant for this mission is hydroxylammonium nitrate (NH 3 OHNO 3) fuel/oxidizer blend, also known as AF-M315E. [6] [10] Preliminary data indicates that it offers nearly 50% higher performance for a given propellant tank volume compared to a conventional monopropellant hydrazine system.

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