SDS |
USA |
Launch data:
|
![]() An isometric view of the SDS as ready for installation aboard the ISS and shown integrated with ESA′s Columbus module External Payload Adapter, but without thermal blankets (image credit: NASA) | ||||||||||||||||||||||
| Prime manufacturer | NASA Goddard Space Flight Center |
| Platform | |
| Operator | NASA's Johnson Space Center in Houston |
| Mass at launch | 363 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | None |
| DC power | |
| Design lifetime | 5 yrs |
![]() The ESA Columbus module′s External EPF-SOX location (image credit: NASA) |
| Ref.: #6 - update: 10.05.19 | Home |