Atlas LV-3B
Launch vehicle · USA
Original archive entry. The text, images and links below are kept as they were written.
American orbital launch vehicle. First operational version of Atlas ICBM and used as launch vehicle for Project Mercury.
LEO Payload: 1,360 kg (2,990 lb) to a 185 km orbit at 28.00 degrees. Flyaway Unit Cost 1985$: 14.210 million. Maximum range: 13,000 km (8,000 mi).
Related
- Family
- orbital launch vehicle
- Country
- USA
- Agency
- Convair