TIVRA L-1380

The TIVRA L-1380 solid rocket motor is engineered for demanding aerospace and experimental rocketry applications requiring high thrust and consistent performance. With a maximum thrust of 4000 N, total impulse of 4000 Newton-seconds, and a 2.5-second burn duration, the motor provides a powerful and stable thrust profile for short-duration high-energy missions. Housed in a 95 mm diameter casing with a 538 mm length, the motor has a total mass of 6 kg, including 3.3 kg of propellant, ensuring an optimal balance between thrust output and structural efficiency. The TIVRA L-1380 is suitable for research institutions, student rocketry teams, and aerospace developers seeking dependable propulsion for flight testing, technology demonstration, and system validation.