"Kysl\u00EDk 20.6 kg/s, vod\u00EDk 3.5 kg/s"@cs . . . "RL-10"@cs . . "RL-10B"@cs . "RL-10A4-2 - 140 kgRL-10B-2 - 277 kg"@cs . "regenerativn\u00ED"@cs . . . . . "Atlas Saturn IDelta IVTitan"@cs . "1959"^^ . . . "RL-10A-3A"@cs . "384241"^^ . "RL-10 je raketov\u00FD motor na kapaln\u00E9 pohonn\u00E9 l\u00E1tky, byl prvn\u00EDm americk\u00FDm motorem spaluj\u00EDc\u00EDm kapaln\u00FD kysl\u00EDk a vod\u00EDk. Byl vyvinut spole\u010Dnost\u00ED Pratt&Whitney na po\u010D\u00E1tku 60. let. Pou\u017E\u00EDval se na druh\u00E9m stupni rakety Saturn I, d\u00E1le na raketov\u00E9m stupni Centaur raket Atlas a Titan a tak\u00E9 v druh\u00E9m stupni raket Delta III a IV."@cs . "500"^^ . "Expanzn\u00ED"@cs . "USA"@cs . . . "16405954"^^ . "RL-10"@cs . "RL-10 je raketov\u00FD motor na kapaln\u00E9 pohonn\u00E9 l\u00E1tky, byl prvn\u00EDm americk\u00FDm motorem spaluj\u00EDc\u00EDm kapaln\u00FD kysl\u00EDk a vod\u00EDk. Byl vyvinut spole\u010Dnost\u00ED Pratt&Whitney na po\u010D\u00E1tku 60. let. Pou\u017E\u00EDval se na druh\u00E9m stupni rakety Saturn I, d\u00E1le na raketov\u00E9m stupni Centaur raket Atlas a Titan a tak\u00E9 v druh\u00E9m stupni raket Delta III a IV."@cs . "LR-119, J-2"@cs . . . . . . . . "5"^^ . . . . . . "700.0"^^ . . . . "6270"^^ . "RL-10A-4-2"@cs . . . . . "RL-10-B2"@cs . "60.53"^^ . "67"^^ . . "1961"^^ . . . . "Motor vy\u0161\u0161\u00EDch stup\u0148\u016F"@cs . . . . . . . "RL-10"@cs . . "Kapaln\u00FD kysl\u00EDk"@cs . . . . . "0.99"^^ . . . . . "RL-10B2"@cs . "Motor RL-10 p\u0159i testech trysky"@cs . "4530"^^ . . "ano"@cs . . . "3.9"^^ . "elektromechanick\u00E9, \u00B14\u00B0"@cs . "ano"@cs . "XLR-115"@cs . "LR-115"@cs . . . . . "RL-10B-2 - Delta IVRL-10A-4-2 - Atlas V"@cs . "1,7 m"@cs . . . . "regulovateln\u00FD, a\u017E 250:1"@cs . . . "LOX/LH2 5:1"@cs . . "aktivn\u00ED"@cs . "RL-10-B"@cs . "RL-10A4-2 - 99 kNRL-10B-2 -110 kN"@cs . . .