NASA / TN D-5597
Niedzwiecki,Richard W
PERFORMANCE OF A 48-MODULE SWIRL-CAN TURBOJET COMBUSTOR SEGMENT AT HIGH TEMPERATURES USING ASTM-A1 FUEL. / .- Nasa, Washington, D.C., 1969 .- 38 .
Bound With Nasa Tn D-5590-96, 5598-99 Lack No.5594
Author Added Entry:
Moyer,Harry M;
Copy Details:
Acc. No.: TR12671, Full Call No.: NASA TN D-5597, Item type: Technical Report , Location: General Stacks,
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Niedzwiecki,Richard W
PERFORMANCE OF A 48-MODULE SWIRL-CAN TURBOJET COMBUSTOR SEGMENT AT HIGH TEMPERATURES USING ASTM-A1 FUEL. / .- Nasa, Washington, D.C., 1969 .- 38 .
Bound With Nasa Tn D-5590-96, 5598-99 Lack No.5594
Author Added Entry:
Moyer,Harry M;
Copy Details:
Acc. No.: TR12671, Full Call No.: NASA TN D-5597, Item type: Technical Report , Location: General Stacks,
------------------------- --------------------- ------ --------- ------- ------- --------- --------