TIP 2, 3 (Triad 2, 3 / NNS) (original) (raw)
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Nova (similar to TIP 2 and 3)
[US Navy]
The TIP 2 and 3 (Transit Improvement Program) satellites used a simplified form of the Triad 1 drag correction system. Pulsed plasma thrusters were used for drag correction maneuvers. The satellites were used operationally in the Transit navigation system. Slightly improved versions were built as Nova.
| Nation: | USA |
|---|---|
| Type / Application: | Navigation |
| Operator: | USN |
| Contractors: | JHU/APL |
| Equipment: | ? |
| Configuration: | Transit-Bus, Gravity Stabilized |
| Propulsion: | Pulsed plasma thrusters |
| Power: | 4 deployable fixed solar arrays, batteries |
| Lifetime: | |
| Mass: | |
| Orbit: | 484 km × 583 km, 90.43� (#2); 343 km × 778 km, 90.32� (#3) |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks |
|---|---|---|---|---|---|
| Triad 2 (TIP 2) | 1975-099A | 12.10.1975 | Va SLC-5 | Scout-D1 | |
| Triad 3 (TIP 3) | 1976-089A | 01.09.1976 | Va SLC-5 | Scout-D1 |
References:
- Robert J. Danchik: An Overview of Transit Development
- The Johns Hopkins University, Space Department: Artificial Earth Satellites Designed And Fabricated By The Johns Hopkins University Applied Physics Laboratory
Further Transit missions:
- Transit 1A, 1B
- Transit 2A
- Transit 3A, 3B
- Transit 4A, 4B
- Transit 5A 1, 2, 3
- Transit 5BN 1, 2, 3
- Transit 5C 1
- Transit 5E 1 (S/N 39)
- Transit 5E 2 (S/N 40)
- Transit 5E 3 (S/N 41)
- Transit 5E 4 (S/N 42)
- Transit 5E 5 (S/N 43)
- Transit-O
- Triad 1 / TIP 1
- Triad 2, 3 / TIP 2, 3
- Nova 1, 2, 3
- Transat