Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
MIHT-4
MIHT solid rocket engine. Start-4. In production. Used in Start-4. Estimated values. First flight 1993. Solid propellant rocket stage. All estimated.

AKA: 15Zh58D. Status: In production. Number: 7 . Thrust: 9.80 kN (2,203 lbf). Gross mass: 1,000 kg (2,200 lb). Unfuelled mass: 300 kg (660 lb). Specific impulse: 295 s. Burn time: 207 s. Height: 2.50 m (8.20 ft). Diameter: 1.40 m (4.50 ft).

People: Nadiradze. Country: Russia. Launch Vehicles: Start-1, Start, Start-1.2. Propellants: Solid. Stages: MIHT-4. Bibliography: 42.
Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use