.. mhf3_prop

MHF3
====




Reference Points
----------------

MHF3 == 86% MMH + 14% N2H4 == MHF-3 == MixedHydrazineFuel-3




`Hover over column headers to see definitions, values to see alternate units`

.. raw:: html

    <table width="100%">
    <tr><th></th>
        <th title="Reference Temperature">Tref</th>
        <th title="Reference Pressure">Pref</th>
        <th title="Specific Gravity">SG</th>
        <th title="Specific Heat">Cp</th>
        <th title="Heat of Vaporization">dHvap</th>
        <th title="Viscosity">Visc</th>
        <th title="Thermal Conductivity">Cond</th>
        <th title="Surface Tension">Surf</th>
    <tr><th>Source</th><th>R</th><th>psia</th><th>g/ml</th><th>BTU/lbm-R</th><th>BTU/lbm</th><th>poise</th><th>BTU/hr-ft-R</th><th>lbf/in</th></tr>


    <tr  style="background-color:#FFFF00"><td><a class="reference external" href="https://pypi.python.org/pypi/rocketprops">RocketProps</a></td><td  title="527.67 degR
    293.15 degK
    68 degF
    20 degC">527.7</td><td  title="14.6959 psia
    0.999997 atm
    1.01325 bar
    0.101325 MPa">14.7</td><td  title="0.894813 SG
    55.8613 lbm/ft**3
    0.0323272 lbm/inch**3
    894.813 kg/m**3">0.8948</td><td  title="0.717663 BTU/lbm/F
    0.718143 cal/g/C
    0.000718143 kcal/g/C
    3004.71 J/kg/K">0.718</td><td  title="370 BTU/lbm
    205.693 cal/g
    0.205693 kcal/g
    860.62 J/g">370.0</td><td  title="0.00941389 poise
    0.941389 cpoise
    0.000941389 Pa*s
    5.27153e-05 lbm/s/inch
    0.189775 lbm/hr/inch
    3.389 kg/hr/m
    0.03389 kg/hr/cm">9.414e-03</td><td  title="0.16074 BTU/hr/ft/delF
    3.72083e-06 BTU/s/inch/delF
    0.00066491 cal/s/cm/delC
    0.066491 cal/s/m/delC
    0.00278198 W/cm/delC">0.1607</td><td  title="0.000203865 lbf/in
    0.0357022 N/m
    35.7022 mN/m
    35.7022 dyne/cm">2.039e-04</td></tr>
    <tr ><td><a class="reference external" href="./_static/AFRPL-TR-69-149Hydrazine fuels.pdf">AFRPL-TR-69-149</a></td><td  title="536.4 degR
    298 degK
    76.73 degF
    24.85 degC">536.4</td><td  title="14.7 psia
    1.00028 atm
    1.01353 bar
    0.101353 MPa">14.7</td><td  title="0.8889 SG
    55.4922 lbm/ft**3
    0.0321135 lbm/inch**3
    888.9 kg/m**3">0.8889</td><td  title="0.7196 BTU/lbm/F
    0.720082 cal/g/C
    0.000720082 kcal/g/C
    3012.82 J/kg/K">0.720</td><td >---</td><td  title="0.0081 poise
    0.81 cpoise
    0.00081 Pa*s
    4.53579e-05 lbm/s/inch
    0.163288 lbm/hr/inch
    2.916 kg/hr/m
    0.02916 kg/hr/cm">8.100e-03</td><td  title="0.159553 BTU/hr/ft/delF
    3.69336e-06 BTU/s/inch/delF
    0.00066 cal/s/cm/delC
    0.066 cal/s/m/delC
    0.00276144 W/cm/delC">0.1596</td><td  title="0.000204167 lbf/in
    0.0357551 N/m
    35.7551 mN/m
    35.7551 dyne/cm">2.042e-04</td></tr>
    <tr ><td><a class="reference external" href="./_static/Aerojet_Propellant_Properties.pdf">Aerojet</a></td><td  title="527.67 degR
    293.15 degK
    68 degF
    20 degC">527.7</td><td  title="14.6959 psia
    0.999997 atm
    1.01325 bar
    0.101325 MPa">14.7</td><td  title="0.894813 SG
    55.8613 lbm/ft**3
    0.0323272 lbm/inch**3
    894.813 kg/m**3">0.8948</td><td  title="0.717728 BTU/lbm/F
    0.718209 cal/g/C
    0.000718209 kcal/g/C
    3004.98 J/kg/K">0.718</td><td  title="370 BTU/lbm
    205.693 cal/g
    0.205693 kcal/g
    860.62 J/g">370.0</td><td  title="0.00940692 poise
    0.940692 cpoise
    0.000940692 Pa*s
    5.26763e-05 lbm/s/inch
    0.189635 lbm/hr/inch
    3.38649 kg/hr/m
    0.0338649 kg/hr/cm">9.407e-03</td><td  title="0.16079 BTU/hr/ft/delF
    3.72198e-06 BTU/s/inch/delF
    0.000665115 cal/s/cm/delC
    0.0665115 cal/s/m/delC
    0.00278284 W/cm/delC">0.1608</td><td >---</td></tr>

    </table>





Fluid Properties
----------------

MHF3 == 86% MMH + 14% N2H4 == MHF-3 == MixedHydrazineFuel-3




`Hover over column headers to see definitions, values to see alternate units`

.. raw:: html

    <table width="100%">
    <tr><th></th>
        <th title="Molecular Weight">MolWt</th>
        <th title="Critical Temperature">Tc</th>
        <th title="Critical Pressure">Pc</th>
        <th title="Critical Density">SGc</th>
        <th title="Critical Compressibility Factor">Zc</th>
        <th title="Normal Boiling Point">Tnbp</th>
        <th title="Melting/Freezing Point">Tmelt</th>
        <th title="Pitzer Acentric Factor">omega</th></tr>
    <tr><th>Source</th><th>g/gmole</th><th>R</th><th>psia</th><th>g/ml</th><th>(-)</th><th>R</th><th>R</th><th>(-)</th></tr>


    <tr  style="background-color:#FFFF00"><td><a class="reference external" href="https://pypi.python.org/pypi/rocketprops">RocketProps</a></td><td>43.412</td><td  title="1076.67 degR
    598.15 degK
    617 degF
    325 degC">1076.7</td><td  title="1373 psia
    93.4271 atm
    94.665 bar
    9.4665 MPa">1373.0</td><td  title="0.301971 SG
    18.8514 lbm/ft**3
    0.0109094 lbm/inch**3
    301.971 kg/m**3">0.3020</td><td>0.2737</td><td  title="653.07 degR
    362.817 degK
    193.4 degF
    89.6667 degC">653.1</td><td  title="394.67 degR
    219.261 degK
    -65 degF
    -53.8889 degC">394.7</td><td>0.25224</td></tr>
    <tr ><td><a class="reference external" href="./_static/AFRPL-TR-69-149Hydrazine fuels.pdf">AFRPL-TR-69-149</a></td><td>43.415</td><td >---</td><td >---</td><td >---</td><td>---</td><td  title="653.04 degR
    362.8 degK
    193.37 degF
    89.65 degC">653.0</td><td  title="394.67 degR
    219.261 degK
    -65 degF
    -53.8889 degC">394.7</td><td>---</td></tr>
    <tr ><td><a class="reference external" href="./_static/Aerojet_Propellant_Properties.pdf">Aerojet</a></td><td>43.412</td><td  title="1076.67 degR
    598.15 degK
    617 degF
    325 degC">1076.7</td><td  title="1373 psia
    93.4271 atm
    94.665 bar
    9.4665 MPa">1373.0</td><td  title="0.301971 SG
    18.8514 lbm/ft**3
    0.0109094 lbm/inch**3
    301.971 kg/m**3">0.3020</td><td>0.2737</td><td  title="653.07 degR
    362.817 degK
    193.4 degF
    89.6667 degC">653.1</td><td  title="394.67 degR
    219.261 degK
    -65 degF
    -53.8889 degC">394.7</td><td>0.25613</td></tr>

    </table>





Vapor Pressure
--------------




.. raw:: html

    <div class="columns">
        <div style="width:75%;float:left" >
    
.. image:: ./_static/MHF3_Psat.png
   :target: ./_static/MHF3_Psat.png
    

.. raw:: html

    </div><div ><br><br>

| RocketProps Selected Curve
| :ref:`Aerojet Source`
| :ref:`AFRPL-TR-69-149 Source`
| :ref:`Wagner Fit Source`


.. raw:: html

    </div></div>
    <div style="clear:both"></div>

    
`Click Image to View Fill Size`


Density
-------




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    <div class="columns">
        <div style="width:75%;float:left" >
    
.. image:: ./_static/MHF3_SG.png
   :target: ./_static/MHF3_SG.png
    

.. raw:: html

    </div><div ><br><br>

| RocketProps Selected Curve
| :ref:`Aerojet Source`
| :ref:`AFRPL-TR-69-149 Source`
| :ref:`Rackett Scaling Source`


.. raw:: html

    </div></div>
    <div style="clear:both"></div>

    
`Click Image to View Fill Size`


Heat Capacity
-------------




.. raw:: html

    <div class="columns">
        <div style="width:75%;float:left" >
    
.. image:: ./_static/MHF3_Cp.png
   :target: ./_static/MHF3_Cp.png
    

.. raw:: html

    </div><div ><br><br>

| RocketProps Selected Curve
| :ref:`Aerojet Source`
| :ref:`Joback Source`
| :ref:`AFRPL-TR-69-149 Source`


.. raw:: html

    </div></div>
    <div style="clear:both"></div>

    
`Click Image to View Fill Size`


Viscosity
---------




.. raw:: html

    <div class="columns">
        <div style="width:75%;float:left" >
    
.. image:: ./_static/MHF3_Visc.png
   :target: ./_static/MHF3_Visc.png
    

.. raw:: html

    </div><div ><br><br>

| RocketProps Selected Curve
| :ref:`Aerojet Source`
| :ref:`Squires Source`
| :ref:`AFRPL-TR-69-149 Source`


.. raw:: html

    </div></div>
    <div style="clear:both"></div>

    
`Click Image to View Fill Size`


Heat of Vaporization
--------------------




.. raw:: html

    <div class="columns">
        <div style="width:75%;float:left" >
    
.. image:: ./_static/MHF3_Hvap.png
   :target: ./_static/MHF3_Hvap.png
    

.. raw:: html

    </div><div ><br><br>

| RocketProps Selected Curve
| :ref:`Aerojet Source`
| :ref:`Pitzer Hvap Source`


.. raw:: html

    </div></div>
    <div style="clear:both"></div>

    
`Click Image to View Fill Size`


Thermal Conductivity
--------------------




.. raw:: html

    <div class="columns">
        <div style="width:75%;float:left" >
    
.. image:: ./_static/MHF3_Cond.png
   :target: ./_static/MHF3_Cond.png
    

.. raw:: html

    </div><div ><br><br>

| RocketProps Selected Curve
| :ref:`Aerojet Source`
| :ref:`Nicola Source`
| :ref:`AFRPL-TR-69-149 Source`


.. raw:: html

    </div></div>
    <div style="clear:both"></div>

    
`Click Image to View Fill Size`



Surface Tension
---------------




    

.. raw:: html

    <div class="columns">
        <div style="width:75%;float:left" >
    
.. image:: ./_static/MHF3_Surf.png
   :target: ./_static/MHF3_Surf.png
    

.. raw:: html

    </div><div ><br><br>

| RocketProps Selected Curve
| :ref:`AFRPL-TR-69-149 Source`
| :ref:`Sastri-Rao Source`
| :ref:`Pitzer Surf Source`


.. raw:: html

    </div></div>
    <div style="clear:both"></div>

    
`Click Image to View Fill Size`