Juno V-B
Launch vehicle · USA
Original archive entry. The text, images and links below are kept as they were written.
The selected sequential staging method selected for the Juno-5.
American orbital launch vehicle. A proposed version of the Juno V for lunar and planetary missions used a Titan I ICBM first stage and a Centaur high-energy third stage atop the basic Juno V cluster. Masses, payload estimated.
LEO Payload: 12,500 kg (27,500 lb) to a 185 km orbit at 28.00 degrees. Payload: 3,500 kg (7,700 lb) to a translunar trajectory. Flyaway Unit Cost 1985$: 73.800 million.
Related
- Family
- orbital launch vehicle
- People
- von Braun
- Country
- USA
- Engines
- LR87-3, H-1 engine, RL-10A-1