TIVRA K-925

The TIVRA K-925 solid rocket motor offers a balance between high thrust output and compact design for advanced experimental and educational aerospace applications. Capable of producing a maximum thrust of 1550 N and a total impulse of 2500 Newton-seconds, the motor features a 2.7-second burn duration that enables strong initial acceleration with stable thrust delivery. With a 94 mm diameter, 383 mm motor length, and a total mass of 4.46 kg including 2.2 kg of propellant, the TIVRA K-925 is well-suited for sounding rockets, subscale launch vehicle testing, and propulsion system validation.