User:JustinTime55/sandbox/Gemini spacecraft infobox
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| Manufacturer | McDonnell Aircraft | ||
|---|---|---|---|
| Country of origin | United States | ||
| Operator | NASA | ||
| Applications | Manned orbital flight | ||
| Specifications | |||
| Launch mass | 7,100 to 8,350 pounds (3,220 to 3,790 kg) | ||
| Crew capacity | 2 | ||
| Dimensions | 18 feet 5 inches (5.61 m) long 10 feet (3.0 m) diameter | ||
| Volume | 90 cubic feet (2.5 m3) | ||
| Power | 2 General Electric fuel cells | ||
| Batteries | 5 silver-zinc batteries for re-entry | ||
| Regime | Low Earth orbit | ||
| Design life | 14 days | ||
| Production | |||
| Status | Retired | ||
| Built | 12 | ||
| Launched | 12 | ||
| Failed | 0 | ||
| Lost | 0 | ||
| Maiden launch | April 8, 1964 | ||
| Last launch | November 11, 1966 | ||
| Last retirement | November 15, 1966 | ||
| Related spacecraft | |||
| Flown with | Agena Docking Target | ||
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| Configuration | |||
 Gemini spacecraft diagram
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