Epoxi |
USA |
International Sat. nº: |
USA satellite nº: |
Launch data:
|
Deep Impact (with Impactor) [Ball] | ||||||||||||||||||
| Prime contractor | Ball Aerospace, JPL |
| Operator | NASA |
| Platform | |
| Mass at launch: | |
| Fly-by spacecraft | 601 kg (86 kg of propellant) |
| Impactor | 372 kg (8 kg of propellant) dim: 1 dia, 1 long |
| Launch Mass | 973 kg |
| Basic shape | Box + panel |
| Dimension | 3.3 x 1.7 x 2.3 2.8 span |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime | |
| Ref.: #7(JR589,621,630,686) - update: 02.11.13 | Home |