The Wayback Machine - https://web.archive.org/web/20161228025835/http://astronautix.com/1/15zh58b.html
15Zh58B

Encyclopedia Astronautica
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
15Zh58B
MITT solid rocket engine. Topol'-M second stage.
See More

AKA: Topol'-M-2. Status: Active. Thrust: 490.00 kN (110,150 lbf). Gross mass: 13,000 kg (28,000 lb). Unfuelled mass: 1,500 kg (3,300 lb). Burn time: 64 s. Height: 6.00 m (19.60 ft). Diameter: 1.55 m (5.08 ft).

Subtopics
MIHT-2 solid rocket engine. Start-2. In production. Used in Start-2. Estimated values. First flight 1993. Solid propellant rocket stage. All estimated except stage gross mass. Start second stage.
People: Nadiradze. Country: Russia. Launch Vehicles: Topol'-M, Bulava. Propellants: Solid. Stages: 15Zh58B.
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
� 1997-2016 Mark Wade - Contact
� / Conditions for Use