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Mercury-Redstone BD was an uncrewed booster development flight in the U.S. Mercury program. It was launched on March 24, 1961, from Launch Complex 5 at Cape Canaveral, Florida. The mission used a boilerplate Mercury spacecraft and Redstone MRLV-5.
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redstone mercury spacecraft mr-2 launch mission mercury-redstone boilerplate booster development flight rocket mr-bd km bd 307 494 mr-3 ocean used
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Mercury-Redstone BD | Apogee | 182.7 kilometres (113.5 mi) | 1.00 | infobox |
| Mercury-Redstone BD | Distance travelled | 494 kilometres (307 mi) | 1.00 | infobox |
| Mercury-Redstone BD | Landing date | March 24, 1961, 17:38:23 (1961-03-24UTC17:38:24Z) UTC | 1.00 | infobox |
| Mercury-Redstone BD | Launch date | March 24, 1961, 17:30 (1961-03-24UTC17:30Z) UTC | 1.00 | infobox |
| Mercury-Redstone BD | Launch mass | 1,141 kilograms (2,515 lb) | 1.00 | infobox |
| Mercury-Redstone BD | Launch site | Cape Canaveral LC-5 | 1.00 | infobox |
| Mercury-Redstone BD | Manufacturer | McDonnell Aircraft | 1.00 | infobox |
| Mercury-Redstone BD | Mission duration | 8 minutes, 23 seconds | 1.00 | infobox |
| Mercury-Redstone BD | Mission type | Test flight | 1.00 | infobox |
| Mercury-Redstone BD | Operator | NASA | 1.00 | infobox |
| Mercury-Redstone BD | Rocket | Redstone MRLV MR-5 | 1.00 | infobox |
| Mercury-Redstone BD | Spacecraft type | Mercury boilerplate | 1.00 | infobox |
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