Двигательная установка. RL 10B-2. [Редактировать]

Двигатель RL 10B-2 является типовым представителем RL 10. По состоянию на 2010 год он обладает наибольшим показателем степени расширения сопла. 

Технические характеристики

#ХарактеристикаЗначение
1Длина, метра4.14
2Тяга, кН110
3Удельный импульс, секунд464
4Время работы, секунд1125
5Масса (сухая), кг277
6Соотношение компонентов топлива5.88
7Степень расширения сопла250
8Диаметер, метра2.21
9Сдвигаемый сопловый насадокесть

Найдено 517 документов по запросу «RL 10B-2». [Перейти к поиску]


Дата загрузки: 2017-03-10
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0.13/5
... and 2 custom TMI stages with RL-10-B2 engines used sequentially.... The TMI stage utilizes 4 or 6 RL-10B-2 LOX/LH2 engines. Per payload..., a single custom TMI stage with RL-10-B2 engines, and one... RL-10B-2 LOX/LH2 engines for the small TMI stage • Option 3.2 uses RL... wet mass is reached Table 2: RL-10B-2 engine parameters used for this... mass for various numbers of RL-10B-2 engines The first step to... based on the use of RL-10B-2 engines, and assuming the tank...



Дата загрузки: 2017-04-08
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0.1/5
Sheet2 Rocket Engines 500 RL-10B-2 RL-60 SSME 450 J-2S RS-68 400 350 RD-180 Vacuum ISP (sec) Kestrel 2 RS-84 Merlin 1c F-1 300 GEM 60 RSRB 250 200 150 100 50 0 10 100 1000 Vacuum Thrust (kN) Page 1 10000 100000 Sheet1 Name Vac Thrust(KN) Vac ISP (sec) Fuel RSRB 11500 267 Solid GEM 60 851 275 Solid F-1 7740 304 Lox/Kerosene Merlin 1c 616 305 Lox/Kerosene Kestrel 2 31 317 Lox/Kerosene RD-180 4152 338 Lox/Kerosene RS-68 3312 420 Lox/LH2 J-2S 1138.5 436 Lox/LH2 SSME 2278 453 Lox/LH2 RL-10B-2 110 462 Lox/LH2 RS-84 5159 335 Lox/Kerosene RL-60 289 470 Lox/LH2 Designer Thiokol Delta 4? Rocketdyne SpaceX SpaceX Glushko Rocketdyne Rocketdyne Rocketdyne Pratt and Whitney Rocketdyne Pratt and Whitney Page 2 Date 1980 2002 1959 2006 2006 1999 1998 1967 1972 1998 2005 2001



Дата загрузки: 2017-03-18
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0.35/5
...$ 74 +(#-, 92) $* -#* ) 22, 4($+) . #40$+(, 7) 6$(/ -) ) $+’C) +$#5$. -8#7) 4’. $&* * ) -$+(, 7) +$* #" ) -) 0$98$(/ ) $ W-, (($q $M / ’(4) 8$RL 10B-2$) 47’4) 6$, 40$#4) $#5$5#&-$, 1, ’2, 92) $* , 82#, 0$5, ’-’47... +(, 7) +=$3 , 8$9) . #3 ) $(/ ) $&* * ) -$+(, 7) +$5#-$(-, 4+* #-(’47$, ++) 3 92) 0$* , 82#, 0+$(#$(/ ) $ T, -(/ ?\ ##4$Y?G$2’9-, (’#4$* #’4($#-$9) 8#40:$$; (/ ) -$0, (, $’40’. , () +$(/ ) $RL 10B-2 ) 47’4) $ * -) +&3 , 928$&+) 0$0) 2’1) -+$GGI $>] $(/ -&+($, ($XQO:X$+) . #40... IV)$#-$ 84 5#&-$ SSME$ ) 47’4) +$ 5#-$ , +. ) 4($ * -#* &2+’#4$ , 40$ , 4$ RL-10B-2$ ) 47’4) $ 5#-$ #4?#-9’($ 3 , 4) &1) -+:$$! / ) $+(-) (. / ) 0$(, 4>$/ , +$9) ) 4$+(-&. (&-, 228$+(-) 47(/ ) 4) 0$5#-$(/ ) $, 00) 0$(/ -&+($ , 40...



Дата загрузки: 2017-01-10
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0.09/5
... the transit vehicle and the RL-10B-2 for the reusable lander. The... uses an RL-10 engine. The RL-10B-2 derivative of the RL-10 has... sizing model 4.7 m/3.05 m 8 2600 s RLL RL-10B-2 Expander LH2/LOX 5.88 466... Eq. (2) is a fit for the RL-10. The shifted historical equations... for the J-2X and the RL-10B-2 are given by Eq. (3) and... the sake of robustness. The RL-10B-2 model has an R2 of... (7) Heritage =nveh ntech P erf ormance = 1 T RL missions year (8) −1 (9) 1 1 (1 − PLOM ) × (1 − PLOC ) (10...



Дата загрузки: 2017-01-30
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0.03/5
... vehicles are the Pratt &Whitney RL-10B2, and the Space Shuttle... 4.8 25 km 2 Turbofan, 2 H2 ramjets 1 RL-10B-2 9,500 kg X-37 III. SRT... of the RL10B-2 engine. Table 4: RL-10B-2 Parameter Thrust Burn Time Starts... the velocity of a stage. The RL-10B-2 engine is only used for... 5628 kg 0.26 425 kg RL-10 Simulation Results A high fidelity... stages) VIII. Technology F-35 X-37B RL-10B-2 F135-PW-100 HRE B787...-Vehicle Propulsion Systems, AIAA, 1996. 6 “RL-10,” Aerospace Guide, http://www... IV,” , No. AIAA-2001-3549. 8 “RL-10 - Specifications,” Space and Tech...



Дата загрузки: 2017-04-08
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0.23/5
... also a LH2/LO2 system with a RL-10B-2 motor. The upper stage provides... GTO Stage Specific Impulse (s) 425 10B) (RL- Mass to GEO (kg) Notes...



Дата загрузки: 2016-12-09
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0.15/5
... .RD-0143, -A .RD-0146 (PW, RL-10A4-1) .RD-0162 .RD-0200... .RD-0145 .RD-0146 (PW, RL-10A41) .8D415K .RD-0149 .RD... .VSU-10 .RD-33 .TVD-10B .TVD-20 .TVD-117 .GTD... .PZL K-16 .PZL -10W (TWD-10B Papin (Papin et Rouilly) ============= .Artefacto... .RL-60 .RL “Cobra” .RLX .RL-10 (LR-10) .RL-10A-1 .RL-10A-3 .RL-10A-3A .RL-10A-4 .RL-10A-4-1 .RL-10A-4-2 .RL-10A-5 .RL-10A...-v9 = Rev. 38 .RL-10B-2 .RL-10B-X .RL-10C .RL-10C-X .RL-50 .RL-60 .RD-180 (Lic...-5 .3-S .K-15 .GTD-350 .TWD-10B (TVD-10B) .PZL-10W .2A, Franklin .4A...



Дата загрузки: 2017-05-20
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0.36/5
...-68 (LH2/LO2). •Stage Stage 2: 1 RL RL-10B-2 10B 2 (LH2/LO2) . •First flight Nov...



Дата загрузки: 2017-03-18
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0.09/5
...) Second Stage Engine RS-68 RL 10B-2 Number of Engines in Stage...) Second Stage Engine RD-180 RL 10A-4-2 Number of Engines in... 711 1 in 222 1 in 222 RL-10 B-2 Engine 1 in 1,406 1 in... Failure Core Booster – Strap-CCB – RL-10 B-2 Engine 1 in 2,564 Vehicle...



Дата загрузки: 2017-01-30
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0.12/5
... the analysis. Historic RS–68, RL–10, and SSME data was... altitude-start or an RL–10. The RL–10 was ruled out... were assumed necessary for the RL– 10A–4–2 engine to meet reliability... be a new design utilizing the RL–10A–4–2 engine modified as discussed...–180 in a 4.3-m core, with four RL–10–4–A engines in the upper... 24,750 1 RL-10B-2 24,750 100.0 44,600 2 RL-10A-4-2 22,300... modified existing engines or designs (RL–10A–4, 73-percent J–2S+, 81... phase of comparison included the RL–10, LR–60, LR–85... LR-60 Exp Exp SBORSC RL-10A RD-180 SRB 4-Seg... ExpExp SBORSC Exp Exp Exp RL-10A RD-180 Engine in... appropriate. Various versions of the RL–10 have more than 2 million... Cuts due to engine anomoly RL-10 35 30 25 RD... Exp LR-60 Exp Exp RL-10A SBORSC RD-180 Figure... Table 6-28. Uncertainty Measures Engine RL–10 LR–60 LR–85... that the SSME and the RL–10 are both operational and... containing the SSME, RS–68, J–2, RL–10, LR–60, and LR...–180 booster engines and four RL–10 upper stage engines, and...–68 booster engines and four RL–10 upperstage engines. Each system... upper stage outfitted with four RL–10 engines (designated LV 2) was... needed to human rate the RL–10 and current vehicle designs... by the MPS and the RL–10. This vehicle was not... a new upper stage with four RL–10 engines (designated LV 4), are... human rating the RS–68, RL–10, and overall vehicle. The.... Critical path items included the RL–10 engine, the MPS, and... various engines (LR–85, J–2, J–2S, RL–10), and • EELV options: Delta..., such as J–2, SSME, and the RL–10. The schedule analysis focused...