NASA  / MEMO 12-11-58E <br/>
Hendricks,Robert C,Ehlers,Robert C <br/>
       EVALUATION OF INJECTOR PRINCIPLES IN A 2400-POUND-THRUST ROCKET ENGINE USINJG LIQUID OXYGEN AND LIQUID AMMONIA 
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 .-  Nasa, Washington, D.C.,  1959 
 .- 33 . 
<br/>Bound With Nasa Memo 12-8-58e-12-10-58e, 12-13-58e-12-29-58e Lack No.12-9-58e, 12-12-58e, 12-14-58e-12-20-58e, 12-25-58e-12-28-58e. 
<br/><U>Author Added Entry: </u><br/>Graham,Robert W;
<br><U>Copy Details:</u><br> Acc. No.: <b>TR14064</b>, Full Call No.: NASA MEMO 12-11-58E,   Item type:  Technical Report , Location: General Stacks, <br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>