
VEP [NASDA]
The Vehicle Evaluation Payload (VEP), renamed Myojo after launch, is a Japanese spacecraft that was launched by an H-2 rocket from the Tanegashima space station. It provided a ranging function as well as functions to measure the acceleration and deformation, in order to confirm the accuracy of the H-2 rocket orbit injection and understand the environment of the payload equipment. It remained attached to the second stage of the H-2 launch vehicle.
| Nation: | Japan |
|---|---|
| Type / Application: | Technology |
| Operator: | NASDA |
| Contractors: | NASDA |
| Equipment: | |
| Configuration: | |
| Propulsion: | |
| Power: | Batteries |
| Lifetime: | |
| Mass: | 2391 kg (without second stage) |
| Orbit: | 449 km × 36261 km, 28.6° |
| Satellite | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|
| VEP (Myojo) | 03.02.1994 | Ta YLP-1 | H-2 | with OREX |