" N-II " or N-2 is an American light-launch vehicle of the Delta family.
| PH N-II | |
|---|---|
 N-II launch vehicle | |
| General information | |
| A country |  Japan |
| Family | Delta |
| Appointment | light class booster |
| Developer |  |
| Manufacturer | Mitsubishi heavy industries |
| Main characteristics | |
| Number of steps | 2-3 |
| Length (with GP) | 35 m |
| Diameter | 2.44 m |
| Starting weight | 132.690 t |
| Type of fuel | liquid |
| Payload mass | |
| • at the DOE | 2,000 kg |
| • at GPO | 730 kg |
| Launch history | |
| condition | decommissioned |
| Launch locations | Tanegashima LA-N |
| Number of starts | eight |
| • successful | eight |
| First start | February 11, 1981 |
| Last run | February 19, 1987 |
Creation History
Design
Launch History
See also
- Antares
- Athena
- Comparison of mid-range launch vehicles
- Minotaur