The RD-0124 (GRAU Index 14D23) is a rocket engine burning liquid oxygen and kerosene in an oxygen-rich staged combustion cycle, developed by the Chemical...
9 KB (738 words) - 05:12, 4 May 2023
Chemical Automatics Design Bureau (section RD-0124)
succeeded by V.S. Rachuk [ru] in 1993, then by Viktor D. Gorokhov [ru] (RD-0124 Chief designer) in 2015. During this time the company designed a wide range...
32 KB (3,590 words) - 03:01, 30 July 2024
combustion cycle used in engine RD-191 derivative engine being developed for the Angara rocket RD-0124 used in the Soyuz-2.1b RD-107 used in the R-7 Semyorka...
30 KB (3,224 words) - 23:24, 28 July 2024
an oxygen-kerosene fuel pair and uses the RD-0124A closed circuit engine created at KBHA based on the RD-0124 engine used on the Soyuz-2 launch vehicles...
12 KB (1,026 words) - 16:40, 24 May 2024
Bureau (KBKhA) began conducting research on converting the RD-0120, RD-0124, RD-0234, RD-0242, RD-0256 engine series of designs to methane-oxygen propellants...
7 KB (777 words) - 04:42, 22 May 2024
of 2015: RD-0110 - Upper stage engine of the Soyuz-U, Soyuz-FG and Soyuz-2.1a RD-0110R - Vernier engine of the Soyuz-2.1v first stage. RD-0124 - Upper...
9 KB (612 words) - 20:38, 4 October 2023
derivative of the Zenit's RD-170. The second stage of the Soyuz 2.1v is the same as the third stage of the Soyuz 2.1b; powered by an RD-0124 engine. Most missions...
12 KB (598 words) - 18:24, 6 September 2024
meters in length. It is powered by a single RD-0124A producing 294 kilonewtons, derived from Block I's RD-0124. URM-2 was first flight tested on Angara 1...
4 KB (362 words) - 11:26, 5 August 2022
vacuum version (giant nozzle) that has an Isp of 380". August 3, 2024. "RD-0124 Engine". KBKha. Retrieved January 7, 2016. "ГКНПЦ имени М.В.Хруничева |...
78 KB (1,944 words) - 20:40, 5 September 2024
on the Atlas III launch vehicles. RD-171 (and its RD-171M successor), -180 and -191 are derivatives of RD-170. RD-0124—a series of oxygen/kerosene engines...
27 KB (2,664 words) - 02:27, 2 September 2024
Block I RD-0110 Thrust 298 kN (67.0 klbf) Specific impulse 330 seconds (3.2 km/s) Chamber pressure 6.8 MPa (986 psi) Improved Block I RD-0124 (11D451)...
27 KB (2,964 words) - 21:01, 12 July 2024
Soyuz-7 (rocket family) (redirect from RD-0169A)
use the KBKhA RD-0164[clarification needed] engine in the core[clarification needed] stages, and a methane version of the KBKhA RD-0124[clarification...
24 KB (1,722 words) - 09:19, 1 September 2024
1964. It is also used on the Soyuz third stage in all models until the RD-0124 debut on the 2.1b. It has flown over 1350 times, and accumulated more than...
12 KB (1,157 words) - 09:34, 19 May 2024
URM-2, uses one KBKhA RD-0124A engine also burning liquid oxygen and kerosene. The RD-0124A is nearly identical to the RD-0124 currently powering the...
51 KB (3,554 words) - 04:15, 12 August 2024
has been impressive. The second stage was expected to sport a pair of RD-0124 engines, currently in use on the Soyuz-2 rocket. Thus, both stages would...
19 KB (1,882 words) - 16:49, 2 June 2024
all the same features as the Soyuz 2.1a, but uses an upgraded engine (RD-0124) on the third stage, which greatly increases specific impulse (326 to 359...
116 KB (4,705 words) - 18:54, 6 September 2024
Missiles Unguided rockets Engines RD-8 RD-9 R-11 R-13 R-15 R-25 R-29 RD-33 RD-45 RD-58 RD-107 RD-117 RD-0120 RD-0124 RD-0146 RD-170 RD-180 RD-191 RD-500...
32 KB (4,044 words) - 22:03, 22 July 2024
303.8 s (2.979 km/s) for APCP (Orbus 6E), 359 s (3.52 km/s) for RP1/LOX (RD-0124) and 465.5 s (4.565 km/s) for LH2/LOX (RL10B-2). Propellant fractions are...
44 KB (5,413 words) - 00:21, 2 September 2024
though its RD-0124A engine was an almost identical derivative of the RD-0124 used on Soyuz-2 rockets. The configuration used for the 1.2pp flight was...
5 KB (583 words) - 12:52, 11 April 2024
189 lb) Propellant mass 25,400 kg (56,000 lb) Powered by A: 1 × RD-0110 B: 1 × RD-0124 Maximum thrust A: 298 kN (67,000 lbf) B: 294.3 kN (66,200 lbf) Specific...
40 KB (2,720 words) - 19:52, 8 July 2024
family that utilizes a RD-0124 engine for the Blok-I stage, rather than the older RD-0110 engine used on the Soyuz-2.1a. The RD-0124 grants 34 more seconds...
27 KB (2,808 words) - 23:52, 1 June 2024
second stage flight. At 288 seconds after launch, the Blok I third stage's RD-0124 engine ignited to begin its burn. During third stage flight, an anomaly...
5 KB (381 words) - 18:52, 17 July 2024
Hamilton's west mountain neighbourhoods. In particular, the Stone Church Rd. Storm Trunk Sewer that drains neighbourhoods on either side of Stone Church...
27 KB (1,478 words) - 08:38, 19 April 2024
ISBN 978-0-7190-7649-7 Collison Black, R.D – Economic Thought and the Irish Question 1817–1870, 1993 (reprint of 1960) ISBN 978-0-7512-0124-6 Anderson, James Pauperism:...
11 KB (1,062 words) - 12:57, 15 May 2024
ISBN 978-0-470-88132-3. W. M. C. Sansen (2006). Analog Design Essentials. Dordrecht: Springer. p. 13 (§0124). ISBN 0-387-25746-2. Electronics portal...
22 KB (2,888 words) - 01:29, 21 March 2024
(Buddha blocking river) maybe Wat Phra Non Nong Phueng Nong Phueng 18.7386, 99.0124 67 ยางหนุ่ม yang num (many yang trees) Wat Kong Sai Nong Phueng 18.7304,...
20 KB (2,224 words) - 02:42, 13 August 2024
drug dependences". Magnesium Research. 21 (1): 5–15. doi:10.1684/mrh.2008.0124 (inactive 31 January 2024). PMID 18557129.{{cite journal}}: CS1 maint: DOI...
41 KB (4,971 words) - 12:24, 8 September 2024
and Adolescent Psychopharmacology. 27 (2): 112–116. doi:10.1089/cap.2016.0124. PMID 27813651. Wilens TE, Morrison NR, Prince J (October 2011). "An update...
134 KB (12,347 words) - 15:37, 8 September 2024
Mediterranean Journal of Social Sciences. 9 (4): 149–155. doi:10.2478/mjss-2018-0124. ISSN 2039-2117. Hisham Yaacob, 2006, Waqf Accounting in Malaysian State...
55 KB (6,352 words) - 18:36, 10 August 2024
Behaviour. 51 (5): 1197. 1996. doi:10.1006/anbe.1996.0124. S2CID 235331320. Kennedy, M.; Gray, R.D. & Spencer H.G. (2000). "The Phylogenetic Relationships...
25 KB (2,894 words) - 05:03, 10 May 2024