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
Angara Briz M stage
Part of Briz stage series Family
N2O4/UDMH propellant rocket stage. Version proposed as Angara upper stage. 8 restarts. Propellant ration 2.0:1.

AKA: Angara Briz M. Status: In development. Thrust: 19.60 kN (4,406 lbf). Gross mass: 6,565 kg (14,473 lb). Unfuelled mass: 1,600 kg (3,500 lb). Specific impulse: 326 s. Burn time: 1,000 s. Height: 2.61 m (8.56 ft). Diameter: 2.50 m (8.20 ft). Span: 2.50 m (8.20 ft).



Country: Russia. Engines: S5.98M. Launch Vehicles: Angara 1.1. Propellants: N2O4/UDMH.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use