The design, performance, equipment, and initial flight test results for the S-520 solid fueled rocket are described. The S-520 carries a 408 kg payload, delivers 28,000 lb thrust, has a specific impulse of 29 sec, attains a velocity of 2.13 km/sec, and can reach 232 km altitude. The first S-520 was 9 m long and 0.524 m in diameter and had a three-stage configuration: engine, recovery test unit
... [Show full abstract] (RCU), and scientific instruments. The RTU contained parachute and flotation systems and a Loran-C locator beacon. The initial flight in September 1981 resulted in a splashdown 320 km downrange, with recovery accomplished within 4 hr of launch. Further flight tests and design upgrades are planned.