Salmi, Reino J. <br/>
       NASA Technical Note: Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines 
 / 
 .- Washington, D.C. : NASA ,  1968 
 .- 27p.. 
.- ( NASA Technical Note National Aeronautics and Space Administration.    
<br/><br/>Bound Volume No.101116 Contents TR 7622-7630<br/><br/><br/> <br/><br/><br/>Technical Note D-4851-4860<br/> 
<br/><u>Subject Headings:</u> <br/>Coaxial Injectors -- Oxygen-Hydrogen Rocket Engine;
<br/><U>Author Added Entry: </u><br/>Wanhainen, John P.;<br/>Hannum, Ned P.;
<br><U>Copy Details:</u><br> Acc. No.: <b>101116</b>, Full Call No.: ,   Item type:  Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN D-4851<br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>