



NASA used this Space Shuttle orbiter concept model in wind tunnel tests to learn about the flight characteristics of the vehicle's shape. Although the orbiter would spend most of its time in space, its aerodynamic shape would affect its passage through the atmosphere during launch and descent. Straight wing designs were considered and tested; however a delta wing design was finally chosen, in part to meet U.S. Air Force requirements for high cross-range maneuverability during final descent. Delta wings meant a heavier orbiter and more surface heating during reentry, but they also permitted the orbiter to glide farther without power to reach a runway. NASA transferred a variety of wind tunnel and concept models to the Museum after settling on the final Space Shuttle design.
| Manufacturer | Rockwell International Corporation (Huntington and Downey, CA) |
| Country of Origin | United States of America |
| Materials | Aluminum, epoxy, clear protective coating, steel |
| Dimensions | 3-D: 54.6 × 34.9 × 20.6cm (1 ft. 9 1/2 in. × 1 ft. 1 3/4 in. × 8 1/8 in.) |
| Credit Line | Transferred from the National Aeronautics and Space Administration |
| Inventory Number | A19760754000 |
Where this page came from
This page was imported from Smithsonian National Air and Space Museum. Released by the Smithsonian Institution under CC0 through Smithsonian Open Access.
Nobody has written it yet — it is the source material at a new address, which is why search engines are asked to skip it and why no one earns from it. It is up for grabs: take it on, and it is yours to rewrite and to earn from.
许可协议: CC0 1.0(公有领域) · 改编自 n2t.net
1
0
0
0

留言






