LK-4

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LK-4

Hydrazine propellant rocket stage. Upper stage for orbital insertion of Shavit or Leolink payloads.

Status: Development ended 2001. Thrust: 402 N (90 lbf). Gross mass: 237 kg (522 lb). Unfuelled mass: 71 kg (156 lb). Specific impulse: 200 s. Burn time: 800 s. Height: 1.30 m (4.20 ft). Diameter: 1.56 m (5.11 ft). Span: 1.56 m (5.11 ft).

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.

Country: Israel. Launch Vehicles: LeoLink LK-1.

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