The S5.92 is a Russian rocket engine, currently used on the Fregat upper stage. S5.92 burns a hypergolic mixture of UDMH and nitrogen tetroxide in the...
4 KB (281 words) - 19:14, 4 October 2023
The S5.98M, also known as the 14D30, is a Russian rocket engine, currently powering the Briz upper stages. It was designed by KB KhIMMASH, the famous Isaev...
5 KB (268 words) - 11:41, 22 February 2024
310 lb) Associated stages Comparable Briz-M, Briz-KM Fregat Powered by S5.92 Maximum thrust 19.85 kN (4,460 lbf) Specific impulse 333.2 seconds Burn...
45 KB (1,594 words) - 15:40, 7 June 2024
mass 930 kg (2,050 lb) Propellant mass 5,250 kg (11,570 lb) Powered by S5.92 Maximum thrust 19.85 kilonewtons (4,460 lbf) Specific impulse 333.2 seconds...
18 KB (1,246 words) - 14:51, 24 May 2024
module of the Burya project. S2.1200 S5.1 S.5.6.0000.0 S5.15 S5.33 S5.33A S5.33M S5.41 S5.44 5D25 S5.57 S5.44 5D25 5D25N S5.83 Rocket engines for ICBM and SLBM...
16 KB (1,334 words) - 17:38, 23 October 2023
Fregat-M: 5,600 kg (12,300 lb) Fregat-MT: 7,100 kg (15,700 lb) Powered by 1 × S5.92 Maximum thrust 19.85 kN (4,460 lbf) Specific impulse 333.2 s (3.268 km/s)...
123 KB (4,950 words) - 13:36, 12 July 2024
funds available, so the pad was abandoned. Following two failures in 1991–92 both caused by the second stage, the Zenit was on the verge of being cancelled...
22 KB (2,201 words) - 22:36, 28 May 2024
mass 930 kg (2,050 lb) Propellant mass 5,250 kg (11,570 lb) Powered by S5.92 Maximum thrust 19.85 kilonewtons (4,460 lbf) Specific impulse 333.2 seconds...
25 KB (517 words) - 14:49, 24 May 2024
Archived from the original on 2016-03-04. Retrieved 2015-08-03. "KVD-1 & S5.92 Brochure" (PDF). KB KhIMMASH. 1998-10-13. Retrieved 2015-08-03. "KVD-1 (left)...
8 KB (578 words) - 13:22, 25 May 2024
Fregat-M: 5,600 kg (12,300 lb) Fregat-MT: 7,100 kg (15,700 lb) Powered by 1 × S5.92 Maximum thrust 19.85 kN (4,460 lbf) Specific impulse 333.2 s (3.268 km/s)...
40 KB (2,720 words) - 19:52, 8 July 2024