Altus Specifications
| Title |
Description |
| Owner |
General Atomics Aeronautical System Inc. and NASA |
| Manufacturer |
General Atomics Aeronautical System Inc. |
| Fuselage Length |
23.6 ft. |
| Wingspan |
55.3 ft. |
| Wing Area |
132 ft. |
| Aspect Ratio |
23.2 |
| Maximum Take-off Weight |
2,150 lbs. |
| Payload |
330 lbs. |
| Maximum Altitude |
68,000 ft. |
| Mission Duration |
30 hrs. |
| Structure |
Composite Construction |
| Engine |
Rotax 912-2T |
| Engine Horsepower |
100 @ 52,000 ft. |
| Propeller |
8.2 ft. in Diameter |
|
