Poređenje orbitalnih raketnih motora

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Ova stranica je nepotpuna lista podataka i specifikacija orbitalnih raketnih motora.

Aktuelni, predstojeći i raketni motori u razvoju

Motor Poreklo Dizajner Vozilo Status Korišćenje Pogon Ciklus napajanja Specifični impuls (s)[a] Potisak (N)[a] Pritisak u komori (bar) Masa (kg) Potisak:​ odnos težine[b] Oksidator:​ odnos goriva
Aeon 1  SAD Relativity Space Terran 1 U razvoju 1st CH4 / LOX Gas generator 310 86,740 (SL)[1]
Aeon 1 Vacuum  SAD Relativity Space Terran 1 U razvoju 2nd CH4 / LOX Gas generator 360 100,085 (SL)[1]
AJ-10-190  SAD Aerojet Space Shuttle, Orion Aktivan Upper N2O4/MMH Pod pritiskom 316[2] 26.689[2] 862[2] 118[2] 2.308
AR1  SAD Aerojet Rocketdyne Beta (potential)[3] U razvoju 1st RP-1 / LOX Staged, oxidizer-rich 2,200,000 (SL)[4] 272
BE-3  SAD Blue Origin New Shepard Aktivan 1st LH2 / LOX Combustion tap-off 490,000[5]
BE-3U  SAD Blue Origin New Glenn U razvoju 2nd LH2 / LOX Expander, open 710,000[5]
BE-4  SAD Blue Origin New Glenn, Vulcan U razvoju 1st CH4 / LOX Staged, oxidizer-rich 2,400,000[6][7] 134[8]
CE-20  Indija LPSC GSLV Mk III Aktivan Upper LH2 / LOX Gas generator 434 196,500 6.000 588 341 505
CE-7.5  Indija LPSC GSLV Mk II Aktivan Upper LH2 / LOX Staged 454[9] 73,500 58 445 1.685
E2  SAD ABL Space Systems RS1 U razvoju 1st RP-1 / LOX Gas generator 53,800[10]
E2 Vacuum  SAD ABL Space Systems RS1 U razvoju 2nd RP-1 / LOX Gas generator 57,800[10]
Engine-2  SAD Launcher Space Rocket-1 U razvoju 1st RP-1 / LOX Staged, oxidizer-rich 327[11]
290 (SL) 		100,000[11] 262
Engine-2 Vacuum  SAD Launcher Space Rocket-1 U razvoju 2nd RP-1 / LOX Staged, oxidizer-rich 365[11] 100,000[11] 262
GEM 63  SAD Northrop Grumman Atlas V Aktivan Booster HTPB Čvrsto gorivo 27.906 (Vac)[12] 1,662,745[13] 49,300 with fuel
GEM 63XL  SAD Northrop Grumman Vulcan U razvoju Booster HTPB Čvrsto gorivo 2.803 (Vac)[14] 2.025.720[13] 53,400 with fuel
Hadley  SAD Ursa Major Technologies GOLauncher 1[15] U razvoju 1st RP-1 / LOX Staged, oxidizer-rich 22,241 (SL)[16]
HM-7B Šablon:Podaci o zastavi Evropska Unija Snecma Ariane 2, 3, 4, 5 ECA Aktivan Upper LH2 / LOX Gas generator 446[17]
310 (SL)[18] 		64,800[17]
43,600 (SL)[18] 		37[17] 165[17] 4.325 5
HyPER-15  Južna Koreja Innospace Hanbit-Nano, -Micro, -Mini U razvoju 1st Paraffin / LOX Električna pumpa 292 150,000[19]
LE-5B  Japan Mitsubishi, JAXA H-IIA,
H-IIB 		Aktivan Upper LH2 / LOX Expander, open 447[20] 137,000 360 269 5.193 5
LE-7A  Japan Mitsubishi, JAXA H-IIA,
H-IIB 		Aktivan 1st LH2 / LOX Staged 438[21]
338 (SL)[21] 		1,098,000
870,000 (SL) 		120 1,800 659 59
LE-9  Japan Mitsubishi, JAXA H-3 U razvoju 1st LH2 / LOX Expander, open 425[22] 147,1000 100 2.400 625 5.9
Lightning 1  SAD Firefly Aerospace Alpha Aktivan 2nd RP-1 / LOX Combustion tap-off 322[23] 70,100[23]
Merlin 1D FT  SAD SpaceX Falcon 9 B5, Heavy Aktivan 1st RP-1 / LOX Gas generator 311 914,000[24]
845,000 (SL)[24] 		108.0[25] 470 1.945[24]
Merlin Vacuum 1D  SAD SpaceX Falcon 9 B5, Heavy Aktivan 2nd RP-1 / LOX Gas generator 348[26] 981,000[27] 236
M10 Šablon:Podaci o zastavi Evropska Unija Avio Vega-E[28] U razvoju Upper[28] CH4 / LOX[28] Expander, closed 362[28] 98,000[28] 34[28]
NewtonThree  SAD Virgin Orbit LauncherOne Aktivan Booster RP-1 / LOX Gas generator[29] 266,893[30]
NewtonFour  SAD Virgin Orbit LauncherOne Aktivan 2nd RP-1 / LOX Gas generator[29] 22,241[30]
NK-33A (AJ26-62),
11D111 / 14D15 		 SSSR JSC Kuznetsov Antares 100, Soyuz-2-1v Aktivan 1st RP-1 / LOX Staged, oxidizer-rich 331[31]
297 (SL) 		1,680,000
1,510,000 (SL) 		145 1,222 1.368
P80 Šablon:Podaci o zastavi Evropska Unija Avio Vega Aktivan 1st HTPB Čvrsto gorivo 280[32] 3,015,000[32] 88 96,000 with fuel
P120 Šablon:Podaci o zastavi Evropska Unija Avio Ariane 6,
Vega-C 		Aktivan Booster, 1st HTPB Čvrsto gorivo 279[33] 4,650,000[33] 105 161,000 with fuel[33]
P230 Šablon:Podaci o zastavi Evropska Unija Avio Ariane 5 Aktivan Booster HTPB Čvrsto gorivo 286[34]
259 (SL) 		6,996,000
5,860,000 (SL) 		69 269,000 with fuel[34]
S139  Indija SDSC PSLV Aktivan 1st HTPB Čvrsto gorivo 269[35] 486,0000 58 160,200
with fuel
Raptor[36]  SAD SpaceX Starship U razvoju

and Testing

1st, 2nd CH4 / LOX Staged, full-flow 350[37]
327 (SL) 		2,500,000 (SL, est.) (goal)[38][39] 330[40] ~1.360 (goal)[41] ≥170 (goal)[41] 36[42]
Raptor Vacuum[36]  SAD SpaceX Starship U razvoju 2nd CH4 / LOX Staged, full-flow 380+[43] 3,000,000[44] 330[40] ~1.360 (goal)[41] ≥120 (goal)[41] 36[42]
RD-0124,
14D23 		 Rusija KBKhA Soyuz-2.1b,
Soyuz-2-1v,
Angara 		Aktivan 2nd, 3rd RP-1 / LOX Staged, oxidizer-rich 359[45] 294,300 160 520 577
RD-0146D  Rusija KBKhA Angara U razvoju Upper LH2 / LOX Expander, closed 470[46] 68,600 59
RD-107A,
14D22 		 Rusija NPO Energomash Soyuz-FG, -2 Aktivan 1st RP-1 / LOX Gas generator 3.202[47]
2.633 (SL) 		1,019,892
839,449 (SL) 		612 1,090 7.853
RD-108A,
14D21 		 Rusija NPO Energomash Soyuz-FG, -2 Aktivan 2nd RP-1 / LOX Gas generator 3.206[47]
2.577 (SL) 		921,825
792,377 (SL) 		555 1,075 7.516
RD-171M,[c] 11D520  Rusija NPO Energomash Soyuz-5, Zenit-2M, -3SL, -3SLB, -3SLBF Aktivan 1st RP-1 / LOX Staged, oxidizer-rich 3.372[48]
3.095 (SL) 		7,904,160
7,256,921 (SL) 		250 9,300 7.957
RD-180  Rusija NPO Energomash Atlas V, III Aktivan 1st RP-1 / LOX Staged, oxidizer-rich 3.384[49]
3.119 (SL) 		4,152,136
3,826,555 (SL) 		2.617 5,480 712 272
RD-181  Rusija NPO Energomash Antares 200 Aktivan 1st RP-1 / LOX Staged, oxidizer-rich 3.392[50]
3.119 (SL) 		2,085,000
1,922,000 (SL) 		2.626 2,200 89
RD-191  Rusija NPO Energomash Angara Aktivan 1st RP-1 / LOX Staged, oxidizer-rich 3.375[51]
3.112 (SL) 		2,084,894
1,922,103 (SL) 		2.626 2,200 8.909
RD-193  Rusija NPO Energomash Soyuz-2-1v U razvoju 1st RP-1 / LOX Staged, oxidizer-rich 3.375[52]
3.112 (SL) 		2,084,894
1,922,103 (SL) 		1,900 10.315
RD-276,
14D14M 		 Rusija NPO Energomash Proton-M Aktivan 1st N2O4 / UDMH Staged, oxidizer-rich 3.158[53]
288 (SL) 		1,831,882
1,671,053 (SL) 		1.685 1,120 1.712
RD-801  Ukrajina Pivdenne/​Pivdenmash Mayak U razvoju 1st RP-1 / LOX Staged, oxidizer-rich 336 [54]
3.007 (SL) 		1,339,255
1,198,608 (SL) 		180 1,630 265
RD-809K  Ukrajina Pivdenne/​Pivdenmash Mayak U razvoju Upper RP-1 / LOX Staged, oxidizer-rich 352 [54] 98,067 330 262
RD-810  Ukrajina Pivdenne/​Pivdenmash Mayak, Zenit U razvoju 1st RP-1 / LOX Staged, oxidizer-rich 3.355 [55]
299 (SL) 		2,104,890
1,876,149 (SL) 		180 2,800 265
RD-843  Ukrajina Pivdenne/​Pivdenmash Vega Aktivan upper N2O4 / UDMH Pod pritiskom 3.155 2,452 204 1.593 20
RD-861K  Ukrajina Pivdenne/​Pivdenmash Cyclone-4M U razvoju 2nd N2O4 / UDMH Gas generator 330 [56] 77,629 207 241
RD-870  Ukrajina Pivdenne/​Pivdenmash Cyclone-4M U razvoju 1st RP-1 / LOX Staged, oxidizer-rich 340 [57]
3.015 (SL) 		876,715
777,667 (SL) 		1.353 2.684
Reaver 1  SAD Firefly Aerospace Alpha Aktivan 1st RP-1 / LOX Combustion tap-off 2.956[23] 184,000[23]
RL-10A-4-2[58]  SAD Aerojet Rocketdyne Atlas IIIB, V Aktivan Upper LH2 / LOX Expander, closed 451 99,195 42 168 6.027 55
RL-10B-2[58]  SAD Aerojet Rocketdyne Delta III, IV, SLS Aktivan Upper LH2 / LOX Expander, closed 4.655 110,093 44 301 3.727 588
RL-10C-1[58]  SAD Aerojet Rocketdyne Delta III, IV, SLS, Vulcan Aktivan Upper LH2 / LOX Expander, closed 450 101,820 44 191 545 55
RS-25  SAD Rocketdyne Space Shuttle, SLS Aktivan 1st LH2 / LOX Staged, fuel-rich 4.523
366 (SL) 		2,279,000
1,860,000 (SL)[59] 		2.064 3,526 5.379
RS-68A[d]  SAD Rocketdyne Delta IV, IV Heavy Aktivan 1st LH2 / LOX Gas generator 411[60]
362 (SL) 		3,558,577
3,135,996 (SL) 		109 6,686 5.431 597
Rutherford  Novi Zeland  SAD Rocket Lab Electron Aktivan 1st RP-1 / LOX Električna pumpa 311 24,900
25,000 (SL) 		35[61] 728 (SL)
Rutherford Vacuum  Novi Zeland  SAD Rocket Lab Electron Aktivan 2nd RP-1 / LOX Električna pumpa 343 25,800[61]
S200  Indija SDSC GSLV Mk III Aktivan Booster HTPB Čvrsto gorivo 2.745[62] 5,150,000[63][64][65] 207,000
with fuel[62]
SCE-200  Indija LPSC GSLV Mk III,
ULV 		U razvoju Upper, main RP-1 / LOX Staged, oxidizer-rich 335
299 (SL) 		2,030,000
1,820,000 (SL) 		180 2.700
SLS Solid Rocket Booster[e]  SAD Orbital ATK SLS U razvoju Booster PBAN Čvrsto gorivo 267 16,000,000 730,000
with fuel
SLV-1  Indija Godrej & Boyce PSLV Aktivan Booster HTPB Čvrsto gorivo 253[66] 502,600 43 10,800
with fuel
SRB-A3  Japan IHI Aerospace,
JAXA 		H-IIA,
H-IIB,
Epsilon 		Aktivan Booster HTPB Čvrsto gorivo 2.836[67] 2,305,000
2,150,000 (SL) 		111 76,600
with fuel
TEPREL-B  Španija PLD Space Miura 1 Aktivan 1st RP-1 / LOX Pod pritiskom 30,200 (SL)
TEPREL-C  Španija PLD Space Miura 5 U razvoju 1st, 2nd RP-1 / LOX Gas-generator 190,000 (SL)
TQ-12[68]  Kina Landspace ZQ-2 Aktivan 1st CH4 / LOX Gas generator 284 667,000 (SL) 101
Vikas (rocket engine)  Indija LPSC PSLV, GSLV, GSLV Mk III Aktivan 2nd, main, booster N2O4 / UDMH Gas generator 262 680,500–804,500
600,500–756,500 (SL) 		530–58.5
Vinci Šablon:Podaci o zastavi Evropska Unija Snecma Ariane 6 U razvoju Upper LH2 / LOX Expander, closed[69] 457[70] 180,000 60 280 6.560 61
Vulcain 2 Šablon:Podaci o zastavi Evropska Unija Snecma Ariane 5 Aktivan 1st LH2 / LOX Gas generator 429[71]
318 (SL)[72] 		1,359,000[71]
939,500 (SL)[72] 		1.173[71] 1,800[71] 7.704
YF-21B  Kina AALPT Long March 2E, 2F, 3 Aktivan Booster, 1st N2O4 / UDMH Gas generator 26.066 (SL)[73] 740,400 (SL)[73]
YF-21C  Kina AALPT Long March 2C, 2D, 3A, 3B, 3C, 4B, 4C Aktivan 1st N2O4 / UDMH Gas generator 2.607 (SL)[73] 740,400 (SL)[73]
YF-25  Kina AALPT Long March 3B, 3C Aktivan Booster N2O4 / UDMH Gas generator 26.066 (SL)[73] 740,400 (SL)[73]
YF-22B  Kina AALPT Long March 2E, 2F Aktivan 2nd N2O4 / UDMH Gas generator 2.980[73] 738,400
YF-22C  Kina AALPT Long March 2C, 2D, 4B, 4C Aktivan 2nd N2O4 / UDMH Gas generator 2.980[73] 742,040
YF-22D  Kina AALPT Long March 3 Aktivan 2nd N2O4 / UDMH Gas generator 2.980[73] 741,400
YF-22E  Kina AALPT Long March 3A, 3B, 3C Aktivan 2nd N2O4 / UDMH Gas generator 2.980[73] 741,400
YF-40  Kina AALPT Long March 4B, 4C Aktivan 3rd N2O4 / UDMH Gas generator 303 103,000
YF-50D  Kina AALPT Long March 3B, 3C, 5, 7 Aktivan Upper N2O4 / UDMH Pod pritiskom 3.155 6,500
YF-73  Kina AALPT Long March 3 Aktivan 3rd LH2 / LOX Gas generator 4.200 44,150
YF-75  Kina AALPT Long March 3A, 3B, 3C Aktivan 3rd LH2 / LOX Gas generator 4.380[73] 78,450
YF-75D  Kina AALPT Long March 5 Aktivan 2nd LH2 / LOX Expander, closed 4.426 88,360 41 265 34 60
YF-77  Kina AALPT Long March 5 Aktivan 1st LH2 / LOX Gas generator 428
3.167 (SL) 		700,000
518,000 (SL) 		102 1,054 50 55
YF-79  Kina AALPT Long March 9 U razvoju 3rd LH2 / LOX Expander, closed 4.552 250,000 70 60
YF-90[74]  Kina AALPT Long March 9 U razvoju 2nd LH2 / LOX Staged, fuel-rich 453 2,200,000 183 4,800 4.674 60
YF-100  Kina AALPT Long March 7, 5 Aktivan 1st RP-1/ LOX Staged, oxidizer-rich 3.351
300(SL) 		1,339,480
1,199,190 (SL) 		180 1,912 64 26
YF-115  Kina AALPT Long March 6, 7 Aktivan 2nd RP-1/ LOX Staged, oxidizer-rich 3.415 182,400 120 25
YF-130  Kina AALPT Long March 9 U razvoju 1st RP-1/ LOX Staged, oxidizer-rich 308 (SL) ~5.000,000(SL) 220 ~6,500 78 262
Zefiro 9A Šablon:Podaci o zastavi Evropska Unija Avio Vega Aktivan 3rd HTPB Čvrsto gorivo 2.952[75] 314,000[75] 75 11,400 with fuel
Zefiro 23 Šablon:Podaci o zastavi Evropska Unija Avio Vega Aktivan 2nd HTPB Čvrsto gorivo 2.875[76] 1,122,000[76] 94 25,935 with fuel
Zefiro 40 Šablon:Podaci o zastavi Evropska Unija Avio Vega-C Aktivan 3rd HTPB Čvrsto gorivo 2.935[77] 1,304,000[77] 115 39,206 with fuel

Penzionisani i otkazani raketni motori

Motor Poreklo Dizajner Vozilo Korišćenje Pogon Ciklus napajanja Specifični impuls (s)[a] Potisak (N)[a] Masa (kg) Potisak:​ odnos težine[f] Pritisak u komori (bar) Oksidator:​ odnos goriva
Aerojet M-1  SAD Aerojet Nova ? 1st, 2nd? LH2 / LOX Gas generator 428 (SL) 6,670,000 9,068 60
Aestus Šablon:Podaci o zastavi Evropska Unija Airbus Defence and Space Ariane 5 G, G+, ES Upper N2O4 / MMH Pod pritiskom 324[78] 30,000 111 276 11 19
Aestus II Šablon:Podaci o zastavi Evropska Unija Airbus Defence and Space Ariane 5 Upper N2O4 / MMH Gas generator 340[79] 55,400 138 410 60 19
Aether  SAD Astra Space Rocket 3.0[80] 2nd RP-1/LOX[81] Električna pumpa
AJ-60A  SAD Aerojet Atlas V Booster HTPB Čvrsto gorivo 275 1,270,000[82]
AJ-260-2  SAD Aerojet S-I stage replacement (proposed) 1st PBAN Čvrsto gorivo 263 s 26,183,755 831,345, with fuel
Delphin  SAD Astra Space Rocket 3.0[83] 1st RP-1/LOX[81] Električna pumpa 27.000[84]
F-1[g]  SAD Rocketdyne Saturn V 1st RP-1 / LOX Gas generator 304
263 (SL) 		7,770,000
6,770,000 (SL) 		8,391 8.227 70 227
F-1A[h][85]  SAD Rocketdyne 1st RP-1 / LOX Gas generator 303
270 (SL) 		8,989,000
8,007,000 (SL) 		9,015 906 80 227
Gamma 2  Velika Britanija Bristol Siddeley Black Arrow 2nd RP-1 / H2O2 Staged, decomposition and combustion 265[86] 68,200 173 4.022 8
Gamma 8  Velika Britanija Bristol Siddeley Black Arrow 1st RP-1 / H2O2 Staged, decomposition and combustion 265[87] 234,800 342 7.001 4.740 8
HM-7A Šablon:Podaci o zastavi Evropska Unija Snecma Ariane 1 3rd LH2 / LOX Gas generator 443[88]
308 (SL) 		61,700 149 422 30 5
J-2  SAD Rocketdyne Saturn V, IB 2nd, 3rd LH2 / LOX Gas generator 421[89]
200 (SL) 		1,033,100
486,200 (SL) 		1,438 7.318 30 55
J-2X  SAD Pratt & Whitney Rocketdyne SLS (proposed) Upper LH2 / LOX Gas generator 448[90] 1.307,78 2,472 5.841 95 55–4.5
Kestrel  SAD SpaceX Falcon 1 Upper RP-1 / LOX Pressure fed 317 31,000 52 65 93
LE-5  Japan Mitsubishi, NASDA H-I Upper LH2 / LOX Gas generator 450[91] 103,000 245 4.287 360 55
LE-5A  Japan Mitsubishi, NASDA H-II Upper LH2 / LOX Expander, open 452[92] 121,500 242 5.119 400 5
LE-7  Japan Mitsubishi, NASDA H-II 1st LH2 / LOX Staged combustion 446[93] 1,078,000
843,500 (SL) 		1,714 6.413 127 59
Merlin 1D  SAD SpaceX Falcon 9 v1.1 1st RP-1 / LOX Gas generator 311[94]
282 (SL)[94] 		723,000 470 158 97 234
Merlin Vacuum 1C  SAD SpaceX Falcon 1, 9 2nd RP-1 / LOX Gas generator 336[95] 413,644[95] 92
RD-0120
11D122 		 SSSR KBKhA Energia 1st LH2 / LOX Staged, fuel-rich 455[96] 1,962,000
1,526,000 (SL) 		3,450 5.780 219
RD-8,
11D513 		 SSSR Pivdenne/​Pivdenmash Zenit 2nd vernier RP-1 / LOX Staged, oxidizer-rich 342 78,450 356 7.747 24
RD-56 (KVD-1)
11D56U 		 Rusija KBKhM GSLV Mk I Upper LH2 / LOX Staged, fuel-rich 462[97] 69,626 282 2.517 559
RD-117
11D511 		 SSSR NPO Energomash Soyuz-U 1st RP-1 / LOX Gas generator 316[98]
253 (SL) 		978,000
778,648 (SL) 		1,100 7.218 542
RD-118
11D512 		 SSSR NPO Energomash Soyuz-U 2nd RP-1 / LOX Gas generator 314[98]
257 (SL) 		1,000,278
818,855 (SL) 		1,100 7.591 597
RD-170[i]11D521[99]  SSSR NPO Energomash Energia 1st RP-1 / LOX Staged, oxidizer-rich 3.372
3.095 (SL) 		7,904,160
7,256,921 (SL) 		9,300 7.957 250
RD-264
11D119 		 SSSR NPO Energomash Dnepr 1st N2O4 / UDMH Staged, oxidizer-rich 318[100]
293 (SL) 		4,521,000 3,600 12.815 206
RD-275
14D14 		 Rusija NPO Energomash Proton-M 1st N2O4 / UDMH Staged, oxidizer-rich 316[101]
287 (SL) 		1,831,882
1,671,053 (SL) 		1,070 1.712 1.600
RD-854
8D612 		 SSSR Pivdenne/​Pivdenmash R-36ORB 3rd N2O4 / UDMH Gas generator
RD-855
8D68M 		 SSSR Pivdenne/​Pivdenmash Tsyklon-2, -3, R-36 1st vernier N2O4 / UDMH Gas generator 328,000 320 6.570 197
RD-856
8D69M 		 SSSR Pivdenne/​Pivdenmash Tsyklon-2, -3 (-4), R-36 2nd vernier N2O4 / UDMH Gas generator 54,230 1.125 7.160 198
RD-861
11D25 		 SSSR Pivdenne/​Pivdenmash Tsyklon-2, -3 3rd N2O4 / UDMH Gas generator 78,710 123 888 21
RD-864
15D177 		 SSSR Pivdenne/​Pivdenmash R-36 (missile), Dnipro 3rd N2O4 / UDMH Gas generator 298–309 8,450–20,200 199 17–41 18
RD-869
15D300 		 SSSR Pivdenne/​Pivdenmash R-36M 3rd N2O4 / UDMH Gas generator 302.3–313 8,580–20,470 196 17–41 18
RS-27A  SAD Rocketdyne Delta 1st RP-1 / LOX Gas generator 302[102]
255 (SL) 		1,054,200 1.091 1.025 49 2.245
Space Shuttle Solid Rocket Booster[j]  SAD Thiokol Space Shuttle, Ares I Booster PBAN / APCP Čvrsto gorivo 268 14,000,000
12,500,000 (SL) 		590,000
with fuel
SRB-A  Japan IHI Aerospace, JAXA H-IIA Booster HTPB Čvrsto gorivo 280[103] 2,250,000 76,400 with fuel
UA1207  SAD United Technologies Titan IV Booster PBAN Čvrsto gorivo 272[104]
245 (SL) 		7,116,000
6,410,400 (SL) 		319,330
with fuel
Viking 2 Šablon:Podaci o zastavi Evropska Unija Snecma Ariane 1 1st N2O4 / UDMH Gas generator 690,000
611,200 (SL) 		776 9.067
Viking 2B Šablon:Podaci o zastavi Evropska Unija Snecma Ariane 2, 3 1st N2O4 / UH 25 Gas generator 643,000 (SL) 776 845
Viking 4 Šablon:Podaci o zastavi Evropska Unija Snecma Ariane 1 2nd N2O4 / UDMH Gas generator 713,000 826 88
Viking 4B Šablon:Podaci o zastavi Evropska Unija Snecma Ariane 2, 3, 4 2nd N2O4 / UH 25 Gas generator 800,000 826 9.876
Viking 5C Šablon:Podaci o zastavi Evropska Unija Snecma Ariane 4 1st N2O4 / UH 25 Gas generator 758,000
678,000 (SL) 		826 9.357
Viking 6 Šablon:Podaci o zastavi Evropska Unija Snecma Ariane 4 Booster N2O4 / UH 25 Gas generator 750,000 826 9.259
Vulcain
HM-60 		Šablon:Podaci o zastavi Evropska Unija Snecma Ariane 5 1st LH2 / LOX Gas generator 439[105]
326 (SL)[106] 		1,113,000[105]
773,200 (SL)[106] 		1,300[106] 8.438 109[105]
Waxwing  Velika Britanija Bristol Aerojet Black Arrow Upper Čvrsto gorivo 278[107]
245 (SL) 		29,400
25,900 (SL) 		87 3.448

Vidi još

Napomene

  1. ↑ 1,0 1,1 1,2 1,3 Na nivou mora ako je označeno SL, inače u vakuumu
  2. ↑ Težina se izračunava pri standardnoj gravitaciji.
  3. ↑ Najmoćniji višekomorni raketni motor na svetu
  4. ↑ Najmoćniji motor na vodonik na svetu
  5. ↑ Najveći, najmoćniji motor na čvrsto gorivo ikada napravljen
  6. ↑ Težina se izračunava pri standardnoj gravitaciji.
  7. ↑ Najmoćniji raketni motor sa jednom komorom na tečno gorivo ikada razvijen
  8. ↑ Testirano, ali nikada nije leteo
  9. ↑ Najmoćniji raketni motor na svetu na tečno gorivo
  10. ↑ Najveći raketni motor na čvrsto gorivo koji je ikada leteo, i prvi koji se koristio za primarni pogon u svemirskim misijama sa ljudskom posadom

Reference

  1. ↑ 1,0 1,1 „Terran 1 Technical Specifications”. Relativity. Pristupljeno 2019-10-05. 
  2. ↑ 2,0 2,1 2,2 2,3 „In-Space Product Data Sheets” (PDF). Aerojet Rocketdyne. September 13, 2019. 
  3. ↑ „Aerojet Rocketdyne and Firefly Aerospace to Provide Flexible Access to Space”. Global Newswire (saopštenje za javnost). October 18, 2019. 
  4. ↑ „AR1 Engine”. Aerojet Rocketdyne. Arhivirano iz originala na datum 2016-03-04. Pristupljeno 2016-10-26. 
  5. ↑ 5,0 5,1 „BE-3”. Blue Origin. 
  6. ↑ Ferster, Warren (2014-09-17). „ULA To Invest in Blue Origin Engine as RD-180 Replacement”. Space News. Arhivirano iz originala na datum September 18, 2014. Pristupljeno 2014-09-19. 
  7. ↑ „BE-4”. Blue Origin. Arhivirano iz originala na datum 17 September 2014. Pristupljeno 17 September 2014. 
  8. ↑ Berger, Eric (2016-03-09). „Behind the curtain: Ars goes inside Blue Origin's secretive rocket factory”. Ars Technica. Pristupljeno 2016-03-09. 
  9. ↑ „GSLV Launch Vehicle Information”. Spaceflight101.com. Arhivirano iz originala na datum January 6, 2014. Pristupljeno 6 January 2014. 
  10. ↑ 10,0 10,1 „RS1”. ABL (na jeziku: engleski). Pristupljeno 2022-08-21. 
  11. ↑ 11,0 11,1 11,2 11,3 „Engine-2”. LAUNCHER (na jeziku: engleski). Pristupljeno 2019-11-09. 
  12. ↑ „NG Prop Catalog” (PDF). 2020-12-10. Arhivirano iz originala (PDF) na datum 2020-12-10. 
  13. ↑ 13,0 13,1 „Developing Vulcan Centaur” (PDF). ULA. April 4, 2019. Arhivirano iz originala (PDF) na datum August 25, 2019. 
  14. ↑ „NG Prop Catalog” (PDF). 2020-12-10. Arhivirano iz originala (PDF) na datum 2020-12-10. 
  15. ↑ „Generation Orbit - 9.28”. TMRO. 2016-09-11. Pristupljeno 2017-05-20 — preko YouTube. 
  16. ↑ „The Engines”. Ursa Major Technologies (na jeziku: engleski). Pristupljeno 2017-05-20. 
  17. ↑ 17,0 17,1 17,2 17,3 „HM-7 and HM-7B Rocket Engine - Thrust Chamber”. Airbus Defence and Space. Arhivirano iz originala na datum 2015-03-18. Pristupljeno 1 November 2015. 
  18. ↑ 18,0 18,1 Wade, Mark. „HM7-B”. Encyclopedia Astronautica. Arhivirano iz originala na datum December 27, 2016. Pristupljeno 10 June 2017. 
  19. ↑ „innospacecorp on Twitter: "Very proud and excited as we get ready to test the world's largest LOx/Paraffin Hybrid rocket engine developed for a smallsat Launcher.The HyPER-15, a 150kN Hybrid rocket engine, is scheduled to test this month at our Geumsan Engine Test Facility. Keep an eye out for our updates!"”. Twitter (na jeziku: engleski). Pristupljeno 2021-07-26. 
  20. ↑ „LE-5B”. Encyclopedia Astronautica. Arhivirano iz originala na datum 27 October 2016. Pristupljeno 13 January 2016. 
  21. ↑ 21,0 21,1 „LE-7A”. Encyclopedia Astronautica. Arhivirano iz originala na datum 28 February 2017. Pristupljeno 13 January 2016. 
  22. ↑ „LE-9” (PDF). 
  23. ↑ 23,0 23,1 23,2 23,3 „Launch-alpha”. Firefly Aerospace (na jeziku: engleski). Pristupljeno 2020-02-02. 
  24. ↑ 24,0 24,1 24,2 „Merlin 1D”. SpaceX. Arhivirano iz originala na datum 6 September 2015. Pristupljeno 26 February 2016. 
  25. ↑ „Evolution of the SpaceX Merlin engine”. www.b14643.de. Pristupljeno 2022-05-08. 
  26. ↑ „SpaceX Falcon 9 Product Page”. Arhivirano iz originala na datum 2014-08-05. Pristupljeno 2015-11-01. 
  27. ↑ „SpaceX”. SpaceX (na jeziku: engleski). Pristupljeno 2020-09-24. 
  28. ↑ 28,0 28,1 28,2 28,3 28,4 28,5 „Motore M10” [Engine M10] (na jeziku: Italian). Avio. Pristupljeno 2021-03-24. 
  29. ↑ 29,0 29,1 Sargent, Scott R.; Noall, Jeff; Becker, Matthew; MacKlin, Scott (2016). „Turbopump Design and Development for the Virgin Galactic Newton Three Engine System”. 52nd AIAA/SAE/ASEE Joint Propulsion Conference. ISBN 978-1-62410-406-0. doi:10.2514/6.2016-4984. 
  30. ↑ 30,0 30,1 „LauncherOne Service Guide” (PDF). Arhivirano iz originala (PDF) na datum 2017-10-22. 
  31. ↑ „NK-33”. Encyclopedia Astronautica. Arhivirano iz originala na datum 25 June 2002. Pristupljeno 30 January 2014. 
  32. ↑ 32,0 32,1 „VEGA: 1° stage - P80 Motor”. Avio.com (na jeziku: engleski). Pristupljeno 2020-01-20. 
  33. ↑ 33,0 33,1 33,2 Press release: Successful first test firing for the P120C solid rocket motor for Ariane 6 and Vega-C
  34. ↑ 34,0 34,1 „P230”. Encyclopedia Astronautica. Arhivirano iz originala na datum 31 December 2011. Pristupljeno 27 December 2011. 
  35. ↑ „PSLV-1”. Arhivirano iz originala na datum 5 August 2014. Pristupljeno 4 April 2014. 
  36. ↑ 36,0 36,1 „Spacex Raptor”. NASA SpaceFlight. 7 March 2014. Pristupljeno 2 July 2015. 
  37. ↑ Musk, Elon (29 September 2017). „Making Life Multiplanetary”. youtube.com. SpaceX. Pristupljeno 29 September 2017. 
  38. ↑ „Raptor 2 generates more than 230 tons of thrust at sea level, up from Raptor 1’s 185 tons”. Twitter. SpaceX. Pristupljeno 11 February 2022. 
  39. ↑ „Probably 250 t-F by end of year”. Twitter. Elon Musk. Pristupljeno 11 February 2022. 
  40. ↑ 40,0 40,1 „Raptor engine just reached 330 bar chamber pressure without exploding!” (na jeziku: engleski). 2020-08-18. 
  41. ↑ 41,0 41,1 41,2 41,3 Elon Musk on Twitter: Max thrust version of Raptor should achieve true T/W > 170. Target is 1.5 ton engine with >260 t-F. Max Isp version should achieve ~380 sec, but T/W probably <120 due to big nozzle. These are just guesses for now.
  42. ↑ 42,0 42,1 Katy Groom; Rebecca Bolt; Resa Cancro; Patrice Hall; Kandi Lawson; Mark Mercadante; Michelle Moore; Jane Provancha; Matthew Thompson; Don Dankert; James Brooks; Daniel Czelusnaik; Eva Long (1 August 2019). „Draft Environmental Assessment for the SpaceX Starship and Super Heavy Launch Vehicle at Kennedy Space Center (KSC)” (PDF). netspublic.grc.nasa.gov (na jeziku: engleski). Space Exploration Technologies Corporation. str. 250. Arhivirano iz originala (PDF) na datum 2 August 2019. Pristupljeno 5 August 2019. 
  43. ↑ „First Private Passenger on Lunar BFR Mission”. YouTube. 17 September 2018. Pristupljeno 18 August 2018. 
  44. ↑ „Starship Update”. Youtube. SpaceX. Pristupljeno 11 April 2020. 
  45. ↑ „RD-0124 Engine”. KBKha. Pristupljeno 7 January 2016. 
  46. ↑ „GKNPC imeni M.V.Hruničeva | Židkostnый raketnый dvigatelь RD - 0146”. www.khrunichev.ru. Pristupljeno 2019-07-27. 
  47. ↑ 47,0 47,1 „RD-107A and RD-108A”. NPO Energomash. Pristupljeno 30 June 2015. 
  48. ↑ „RD-171M”. NPO Energomash. Pristupljeno 30 June 2015. 
  49. ↑ „RD-180”. NPO Energomash. Pristupljeno 30 June 2015. 
  50. ↑ „Antares 200 Series – Rockets”. 
  51. ↑ „RD-191”. NPO Energomash. Pristupljeno 30 June 2015. 
  52. ↑ „Universalьnый raketnый dvigatelь RD-193. Mnenie inženera-razrabotčika”. Žurnal «Novosti kosmonavtiki». 
  53. ↑ „RD-276 "Comrade"”. NPO Energomash. Pristupljeno 14 October 2019. 
  54. ↑ 54,0 54,1 „RD-801”. www.yuzhnoye.com. Pristupljeno 2020-01-19. 
  55. ↑ „RD-810”. www.yuzhnoye.com. Pristupljeno 2020-01-19. 
  56. ↑ „RD-861K”. www.yuzhnoye.com. Pristupljeno 2020-01-19. 
  57. ↑ „RD-870”. Yuzhnoye SDO. Pristupljeno 2020-01-19. 
  58. ↑ 58,0 58,1 58,2 „RL10 Data Sheet-1” (PDF). Feb 2016. Arhivirano iz originala (PDF) na datum July 5, 2016. Pristupljeno March 23, 2019. 
  59. ↑ Aerojet Rocketdyne, RS-25 Engine Archived 2015-12-29 at the Wayback Machine. (accessed July 22, 2014)
  60. ↑ „RS-68A”. www.rocket.com. Pristupljeno 19 January 2020. 
  61. ↑ 61,0 61,1 „Rocket Lab Increases Electron Payload Capacity, Enabling Interplanetary Missions and Reusability”. Rocket Lab (na jeziku: engleski). Pristupljeno 26 October 2020. 
  62. ↑ 62,0 62,1 „LVM3”. Arhivirano iz originala na datum 10 September 2015. Pristupljeno 21 December 2014. 
  63. ↑ „ISRO Press Release: S200 First Static Test (S-200-ST-01)” (PDF). Arhivirano iz originala (PDF) na datum 2013-03-11. Pristupljeno 2015-09-25. 
  64. ↑ „Isro successfully tests world's 3rd largest solid booster”. dna. Pristupljeno 4 October 2014. 
  65. ↑ „India to test world's third largest solid rocket booster”. Science and Technology Section. The Hindu News Paper. 2009-12-07. Pristupljeno 2009-12-07. 
  66. ↑ „SLV-1”. Arhivirano iz originala na datum 5 August 2014. Pristupljeno 4 April 2014. 
  67. ↑ „SRB-A3”. Spaceflight101. Pristupljeno 13 January 2016. 
  68. ↑ “天鹊”80吨液氧甲烷发动机100%推力100秒试车圆满成功
  69. ↑ „Vinci”. Encyclopedia Astronautica. Arhivirano iz originala na datum October 27, 2016. Pristupljeno 10 June 2017. 
  70. ↑ „Vinci® engine” (PDF). Ariane. Pristupljeno 10 October 2022. 
  71. ↑ 71,0 71,1 71,2 71,3 „Vulcain Astrium”. Airbus Defence and Space. Arhivirano iz originala na datum 2012-03-27. Pristupljeno 27 December 2011. 
  72. ↑ 72,0 72,1 „Vulcain 2”. Encyclopedia Astronautica. Arhivirano iz originala na datum December 28, 2016. Pristupljeno 27 December 2011. 
  73. ↑ 73,00 73,01 73,02 73,03 73,04 73,05 73,06 73,07 73,08 73,09 73,10 „2.2 LM-3A Launch Vehicle”. LM-3A Series Launch Vehicle User's Manual. Issue 2011 (PDF). CASC. 2011. str. 2—4. Pristupljeno 2016-01-16. 
  74. ↑ 孙纪国,郑孟伟,龚杰峰,陶瑞峰 (2022-01-15). „220tf补燃循环氢氧发动机研制进展” (na jeziku: kineski). 《火箭推进》2022年02期. Pristupljeno 2022-06-05. 
  75. ↑ 75,0 75,1 „VEGA C: 3° stage - zefiro 9”. Avio.com (na jeziku: engleski). Pristupljeno 2020-01-20. 
  76. ↑ 76,0 76,1 „VEGA: 2° stage - zefiro 23”. Avio.com (na jeziku: engleski). Pristupljeno 2020-01-20. 
  77. ↑ 77,0 77,1 „Zefiro 40 Motor Main Characteristics”. Avio.com (na jeziku: engleski). Pristupljeno 2021-05-24. 
  78. ↑ „Aestus Rocket Engine”. Airbus Defence and Space. Arhivirano iz originala na datum 2015-04-20. Pristupljeno 29 January 2014. 
  79. ↑ „Aestus Rocket Engine”. Airbus Defence and Space. Arhivirano iz originala na datum 2015-05-28. Pristupljeno 29 January 2014. 
  80. ↑ By (2020-02-28). „Astra Readies Secretive Silicon Valley Rocket; Firm Exits Stealth Mode, Plans Test Launch”. Hackaday (na jeziku: engleski). Pristupljeno 2020-07-03. 
  81. ↑ 81,0 81,1 „Astra Space Rocket”. www.spacelaunchreport.com. Pristupljeno 2020-07-03. 
  82. ↑ „Atlas V Solid Rocket Motor”. Aerojet Rocketdyne. Arhivirano iz originala na datum 2017-03-14. Pristupljeno 2015-06-02. 
  83. ↑ „Astra scrubs DARPA launch challenge attempt”. NASASpaceFlight.com (na jeziku: engleski). 2020-03-02. Pristupljeno 2020-07-03. 
  84. ↑ Berger, Eric (2020-02-06). „At Astra, failure is an option”. Ars Technica (na jeziku: engleski). Pristupljeno 2020-07-03. 
  85. ↑ Alternate Propulsion Subsystem Concepts NAS8-39210 DCN 1-1-PP-02147
  86. ↑ „Gamma 2”. Encyclopedia Astronautica. Arhivirano iz originala na datum 22 May 2013. Pristupljeno 26 April 2013. 
  87. ↑ „Gamma 8”. Encyclopedia Astronautica. Arhivirano iz originala na datum 22 May 2013. Pristupljeno 26 April 2013. 
  88. ↑ Wade, Mark. „HM7-A”. Encyclopedia Astronautica. Arhivirano iz originala na datum December 21, 2016. Pristupljeno 10 June 2017. 
  89. ↑ Wade, Mark. „J-2”. Encyclopedia Astronautica. Arhivirano iz originala na datum July 19, 2016. Pristupljeno 23 December 2011. 
  90. ↑ „J-2X Engine”. Pratt & Whitney Rocketdyne. Arhivirano iz originala na datum 2012-01-03. Pristupljeno 23 December 2011. 
  91. ↑ „LE-5”. Encyclopedia Astronautica. Arhivirano iz originala na datum 27 October 2016. Pristupljeno 13 January 2016. 
  92. ↑ „LE-5A”. Encyclopedia Astronautica. Arhivirano iz originala na datum 11 March 2016. Pristupljeno 13 January 2016. 
  93. ↑ „LE-7”. Encyclopedia Astronautica. Arhivirano iz originala na datum 11 March 2016. Pristupljeno 13 January 2016. 
  94. ↑ 94,0 94,1 „Merlin section of Falcon 9 page”. SpaceX. Arhivirano iz originala na datum 2013-07-15. Pristupljeno 2012-10-16. 
  95. ↑ 95,0 95,1 „Falcon 9 Space Launch Report”. SpaceLaunchReport. Pristupljeno 2015-11-01. 
  96. ↑ „RD0120”. KBKhA. 
  97. ↑ „KVD1 Rocket Engine” Dvigatelь KVD1 (na jeziku: ruski). KBHM im. A.M. Isaeva. 
  98. ↑ 98,0 98,1 „RD-117”. Liquid Propellant Rocket Engines. Arhivirano iz originala na datum 26 August 2012. Pristupljeno 27 November 2012. 
  99. ↑ „RD-170”. Encyclopedia Astronautica. Arhivirano iz originala na datum August 8, 2016. Pristupljeno 24 September 2019. 
  100. ↑ Wade, Mark. „RD-264”. Encyclopedia Astronautica. Arhivirano iz originala na datum October 14, 2016. Pristupljeno 10 June 2017. 
  101. ↑ „RD-253 and RD-275”. NPO Energomash. Arhivirano iz originala na datum April 5, 2015. Pristupljeno 30 June 2015. 
  102. ↑ „RS-27A”. Encyclopedia Astronautica. Arhivirano iz originala na datum August 25, 2016. Pristupljeno 2 November 2021. 
  103. ↑ „SRB-A”. Encyclopedia Astronautica. Arhivirano iz originala na datum March 1, 2002. Pristupljeno 13 January 2016. 
  104. ↑ „UA1207”. Encyclopedia Astronautica. Arhivirano iz originala na datum 4 March 2016. Pristupljeno 27 December 2015. 
  105. ↑ 105,0 105,1 105,2 „Vulcain Astrium”. Airbus Defence and Space. Arhivirano iz originala na datum 2012-02-25. Pristupljeno 27 December 2011. 
  106. ↑ 106,0 106,1 106,2 „Vulcain”. Encyclopedia Astronautica. Arhivirano iz originala na datum December 28, 2016. Pristupljeno 27 December 2011. 
  107. ↑ „Black Arrow-3”. Encyclopedia Astronautica. Arhivirano iz originala na datum December 28, 2016. Pristupljeno 26 April 2013. 
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