The RL10 is a liquid-fuel cryogenic rocket engine built in the United States by Aerojet Rocketdyne that burns cryogenic liquid hydrogen and liquid oxygen...
40 KB (2,901 words) - 04:18, 31 August 2024
Common Centaurs were propelled by the RL10-A-4-2 version of the RL-10. Since 2014, Common Centaur has flown with the RL10-C-1 engine, which is shared with...
38 KB (3,691 words) - 15:44, 12 August 2024
up. Some examples of an expander cycle engine are the Aerojet Rocketdyne RL10 and the Vinci engine for Ariane 6. This operational cycle is a modification...
14 KB (1,373 words) - 23:53, 15 August 2024
continued to use the Centaur upper stage, available with single or dual RL10 engines. The Atlas V, currently in service, was developed by Lockheed Martin...
31 KB (2,625 words) - 06:23, 15 July 2024
merged with Aerojet to form Aerojet Rocketdyne. Pratt & Whitney Rocketdyne RL10 (LH2/LOX) An American Society of Mechanical Engineers (ASME) Historic Landmark...
6 KB (417 words) - 02:54, 22 August 2024
150 s Fuel: RP-1 / LOX The S-IV stage was powered by six LOX / LH2-fueled RL10 engines, mounted on gimbals. The propellant tanks used a single, common bulkhead...
41 KB (5,196 words) - 23:09, 27 July 2024
improved version of the Centaur III used on the Atlas, which is powered by two RL10 engines built by Aerojet Rocketdyne, fueled by liquid hydrogen and liquid...
58 KB (5,326 words) - 01:59, 21 August 2024
List of minor planets: 5001–6000 (redirect from 1988 RL10)
14, 1988 Haute-Provence E. W. Elst ITH 12 km MPC · JPL 5233 Nastes 1988 RL10 Nastes September 14, 1988 Cerro Tololo S. J. Bus L5 29 km MPC · JPL 5234...
232 KB (302 words) - 16:54, 15 August 2024
international customers. RL10 cryogenic flow control valves Atec has manufactured, assembled, and tested cryogenic flow control valves for the RL10 liquid-fueled...
17 KB (1,553 words) - 09:18, 21 March 2022
2, 1978 La Silla C.-I. Lagerkvist KOR 5.1 km MPC · JPL 9267 Lokrume 1978 RL10 Lokrume September 2, 1978 La Silla C.-I. Lagerkvist KOR 5.2 km MPC · JPL...
218 KB (301 words) - 06:14, 28 June 2024
the Aerojet Rocketdyne RL10, providing improved performance and efficiency while maintaining the installation envelope of the RL10. RL60 was planned to...
10 KB (1,092 words) - 04:42, 6 May 2023
Lunar Module Ascent Engine - used on the Apollo Lunar Module's Ascent Stage RL10 - Ubiquitous LOX/LH2 expander cycle engine Kuhr, Jack (2024-03-06). "Blue...
6 KB (452 words) - 12:46, 22 August 2024
2016, it was reported that NASA has chosen to use a design based on four RL10-C3 engines for the EUS, and in October 2016 NASA confirmed they had ordered...
12 KB (935 words) - 02:32, 31 August 2024
extension that is extended during flight, similar to the one found on the RL10 The MARC-60's (then MB-60) development program was announced on 14 February...
8 KB (773 words) - 03:46, 7 August 2022
Tim Dodd Dodd with RL10 rocket engine in June 2021 Born (1985-02-27) February 27, 1985 (age 39) Iowa, United States Nationality American Occupation Science...
7 KB (590 words) - 01:56, 9 August 2024
Jordaens 1988 PR1 Jacob Jordaens, Flemish painter MPC · 5232 5233 Nastes 1988 RL10 Nastes, from Greek mythology. With his brother Amphimacus, he was a leader...
172 KB (470 words) - 19:58, 30 August 2024
with four RL10 engines, two MARC-60 engines, or one J-2X engine. In 2014, NASA also considered using the European Vinci instead of the RL10, which offered...
202 KB (16,126 words) - 01:37, 1 September 2024
Archived from the original on February 25, 2022. Retrieved January 19, 2020. "RL10 Data Sheet-1" (PDF). February 2016. Archived from the original (PDF) on July...
78 KB (1,944 words) - 01:34, 25 August 2024
liquid oxygen. The Centaur upper stage is powered by one or two American RL10 engine(s) manufactured by Aerojet Rocketdyne and burns liquid hydrogen and...
127 KB (8,945 words) - 18:06, 30 August 2024
and military customers for more than four decades. Products included the RL10, the upper stage rocket engine used on the Boeing Delta and Lockheed Martin...
36 KB (3,368 words) - 15:52, 18 August 2024
PT5 T34 XT45 T52 XT57 T73 T800-APW† T900† Propfans 578-DX† Rocket engines RL10 Aeroderivative gas turbine engines GG3/FT3 GG4/FT4 FT8 Subsidiaries Pratt...
12 KB (1,319 words) - 05:04, 28 December 2023
Under the new plan, Vulcan's upper stage is the Centaur V, with two LH2/LOX RL10 engines and no IVF or other ACES extended-duration technology as had been...
16 KB (1,672 words) - 05:55, 3 April 2024
(Hughes HME-5118ME system) NATO Air Defence Ground Environment (NADGE) system RL10 rocket engines Civil NAS (National Airspace System) Air Traffic Control APG-70...
15 KB (1,408 words) - 16:50, 12 August 2023
expendable version, RS-25E will be developed for follow-on SLS launches. RL10 (LH2/LOX) – Developed by Pratt & Whitney and currently used on the Centaur...
28 KB (2,780 words) - 21:58, 14 August 2024
PT5 T34 XT45 T52 XT57 T73 T800-APW† T900† Propfans 578-DX† Rocket engines RL10 Aeroderivative gas turbine engines GG3/FT3 GG4/FT4 FT8 Subsidiaries Pratt...
74 KB (7,302 words) - 21:35, 16 August 2024
Block 1B configuration will add the Exploration Upper Stage, powered by four RL10 engines, to increase payload capacity. An eventual Block 2 variant will upgrade...
96 KB (9,721 words) - 01:41, 31 August 2024
PT5 T34 XT45 T52 XT57 T73 T800-APW† T900† Propfans 578-DX† Rocket engines RL10 Aeroderivative gas turbine engines GG3/FT3 GG4/FT4 FT8 Subsidiaries Pratt...
8 KB (734 words) - 03:53, 9 March 2024
PT5 T34 XT45 T52 XT57 T73 T800-APW† T900† Propfans 578-DX† Rocket engines RL10 Aeroderivative gas turbine engines GG3/FT3 GG4/FT4 FT8 Subsidiaries Pratt...
20 KB (2,419 words) - 12:30, 27 August 2024
30,700 kg (67,700 lb) Propellant mass 27,220 kg (60,010 lb) Powered by 1 RL10-B-2 Maximum thrust 110 kN (25,000 lbf) Specific impulse 465.5 s (4.565 km/s)...
17 KB (1,506 words) - 04:08, 10 July 2024
PT5 T34 XT45 T52 XT57 T73 T800-APW† T900† Propfans 578-DX† Rocket engines RL10 Aeroderivative gas turbine engines GG3/FT3 GG4/FT4 FT8 Subsidiaries Pratt...
17 KB (1,908 words) - 02:28, 5 August 2024