The Wayback Machine - https://web.archive.org/web/20161227222713/http://astronautix.com/b/burya.html
Burya

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

Burya
Part of Burya La-350 Family
Ramjet missile stage. Boosted by 2 x R-11 derivative boosters. 6,500 km tested, 8,000 km specified, cruise at Mach 3.2 at 18-20 km altitude with 2,350 kg warhead. Flight tested 1957 - 1960. Wing area 60 square meters; diameter of ramjet inlet 1.7 m. Total missile mass 97,215 kg; gross masses prorated, empty masses estimated.

AKA: La-X; La-X, Objekt 350. Status: Retired 1960. Payload: 2,350 kg (5,180 lb). Thrust: 76.00 kN (17,085 lbf). Gross mass: 40,865 kg (90,091 lb). Unfuelled mass: 13,000 kg (28,000 lb). Specific impulse: 1,500 s. Burn time: 8,500 s. Height: 18.00 m (59.00 ft). Diameter: 2.20 m (7.20 ft). Span: 7.75 m (25.41 ft). Location: 945.

Release velocity: 945 m/s (3,100 ft/sec). Release altitude: 19 m (62 ft). Release conditions: 3,200 kph at 19 km.

Country: Russia. Engines: RD-012U. Launch Vehicles: Burya La-350. Propellants: Air/Kerosene. More at: 9639.



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