LK-4
Stage · Israel
Original archive entry. The text, images and links below are kept as they were written.
Hydrazine propellant rocket stage. Upper stage for orbital insertion of Shavit or Leolink payloads.
Subtopics
- RSA-4-4 Hydrazine propellant rocket stage. Specific impulse estimated. Maximum propellant load indicated (hydrazine monopropellant contained in 4 x 50 l tanks). Upper stage used for orbit circularization at apogee, dispensing of dual payloads, third station nutation damping. Equipped with 2 x 200 N engines for maneuver, 4 x 200 N for roll control, and 4 x 25 N for yaw and pitch.
Related
- Country
- Israel
- Launch Vehicles
- LeoLink LK-1