LANDING CHRACTERISTICS OF THE APOLLO SPACECRAFT WITH DEPLOYED-HEAT-SHIELD IMPACT ATTENUATION SYSTEMS.
By: Stubbs,Sandy M.
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-3059 (Browse shelf) | Not for loan | TR15320 |
Total holds: 0
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Bound With Nasa Tn D-3051-3058,3060.
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