NASA / MEMO 4-23-59L
Lundstrom,Reginald R
ANALYTICAL INVESTIGATION OF A FLIKER-TYPE ROLL CONTROL FOR A MACH NUMBER 6 MISSILE WITH AERODYNAMIC CONTROLS OVER AN ALTITUDE RANGE OF 82,000 TO 282,000 FEET
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.- Nasa, Washington, D.C., 1959
.- 50 .
Bound With Nasa Memo 4-20-59l -4-22-59l And 4-30-59l Lack No.24-29
Author Added Entry:
Whitman,Ruth I;
Copy Details:
Acc. No.: TR7402, Full Call No.: NASA MEMO 4-23-59L, Item type: Technical Report , Location: General Stacks,
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