EMPIRICAL METHOD FOR DETERMINING STATIC DISTRIBUTED AERODYNAMIC LOADS ON AXISYMMETRIC MULTISTAGE LAUNCH VEHICLES
By: Muraca,Ralph J.
Material type:![materialTypeLabel](/opac-tmpl/lib/famfamfam/BK.png)
Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
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PK Kelkar Library, IIT Kanpur | General Stacks | NASA TN D-3283 - (Browse shelf) | Not for loan | TR10032 |
Total holds: 0
Bound With Nasa Tn D-3281-90
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