MIHT solid rocket engine. 9.8 kN. Start-4. In production. Used in Start-4. Estimated values. Isp=295s. First flight 1993.
Application: Start-4.
Status: In production.
Gross mass: 1,000 kg (2,200 lb).
Unfuelled mass: 300 kg (660 lb).
Height: 2.50 m (8.20 ft).
Diameter: 1.40 m (4.50 ft).
Thrust: 9.80 kN (2,203 lbf).
Specific impulse: 295 s.
Burn time: 207 s.
Number: 7 .
More... - Chronology...
Associated Countries
See also
Associated Launch Vehicles
-
Start-1 Russian orbital launch vehicle. Launch vehicle based on decommissioned ICBM's. Launched from mobile transporter. Liftoff mass 47 tonnes. More...
-
Start Russian orbital launch vehicle. Launch vehicle based on decommissioned SS-25 ICBM's (differs from ICBM/basic Start-1 in having second stage used twice, in tandem, for increased payload). Launched from mobile transporter. Liftoff mass 60 tonnes. More...
Associated Manufacturers and Agencies
-
Nadiradze Russian manufacturer of rocket engines and rockets. Nadiradze, Russia. More...
Associated Propellants
-
Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...
Bibliography
-
Isakowitz, Steven J,, International Reference to Space Launch Systems Second Edition, AIAA, Washington DC, 1991 (succeeded by 2000 edition).
Associated Stages
-
MIHT-4 Solid propellant rocket stage. Loaded/empty mass 1,000/300 kg. Thrust 9.80 kN. Vacuum specific impulse 295 seconds. All estimated More...
Home - Browse - Contact
© / Conditions for Use
