Patch, R W. <br/><br/>
Thermodynamics properties and theoretical rocket performance of hydrogen to 100000 K and 1.01325x10^8 N/m^2 / 

 - Washington D C :   National Aeronautics and Space Administration,   1971. 
 - 111 p. :  ill. ;  27 cm. 
 - National Aeronautics and Space Administration special publication  3069 .
<br/><br/>Includes bibliographic references. 
<br/><br/><label>Subjects--Topical Terms: </label><br/>High-temperature thermodynamics<br/>Rocket fuels--Hydrogen<br/>Compressible flow--Rocket propulsion
<br/><br/><label>Dewey Class. No.: </label>536.7  / PAT