Convair X-11
From Wikipedia, the free encyclopedia
The Convair X-11 (originally designated the Convair XSM-16A) was the first testbed for what became the Atlas missile program. Later the Convair X-12 became the second, more advanced testbed for the Atlas program.
[edit] Service history
A total of 12 X-11's were built and tested. The first three were involved in static tests only. X-11 Number 4 and 6, were destroyed in launch accidents. All others performed successful test flights. The test series began on June 11, 1957 and ended on June 3, 1958.
[edit] Specifications (X-11)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.Data from {name of first source}
General characteristics
- Crew: Unmanned
- Length: 96 ft (29.3 m)
- Wingspan: 12 ft (3.66 m)
- Height: ()
- Empty weight: 12,500 lb (5,670 kg)
- Loaded weight: 80,000 lb (36,300 kg)
- Powerplant: 1× rocket engine
Performance
- Maximum speed: Mach 10+
- Range: 600 nm (690 mi, 1,110 km)
- Service ceiling 40 mi (60 km)
[edit] See also
Related lists
|
||||||||
|
|||||
|
||||||||||||||
