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Arcjet rocket

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931: 100:-powered arcjet engines capable of power outputs from 1 to 100 kW. The heated hydrogen reaches exit speeds of 16 kilometres per second (9.9 mi/s). An arcjet-propelled test satellite by the name of 55:). This imparts additional energy to the propellant, so that one can extract more work out of each kilogram of propellant, at the expense of increased power consumption and (usually) higher cost. Also, the 157: 226: 265: 142: 661: 198: 779: 400: 36: 677: 238: 258: 582: 656: 682: 547: 251: 786: 641: 610: 605: 195: 104:(BW1) was scheduled to go to the Moon by 2010. No such launch has yet occurred. Baden-Württemberg 1 would have used 96:'s Institute of Space Aviation Systems have been looking into these challenges for years and have developed various 955: 741: 600: 774: 533: 507: 449: 433: 423: 830: 803: 758: 746: 726: 492: 454: 428: 220:(Arcjet propulsion systems for space applications), Prof. Monika Auweter-Kurtz, B.G. Teubner Stuttgart 1992 105: 93: 881: 731: 631: 373: 101: 158:"Lockheed Martin Awards Aerojet Rocketdyne Contract to Provide Propulsion Subsystems on A2100 Satellites" 466: 459: 274: 74: 63: 577: 572: 476: 390: 40: 736: 721: 636: 523: 502: 471: 62:
When the energy is available, arcjets are well suited to keeping stations in orbit and can replace
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John, R. R., Bennett, S., and Connors, J. P., "Arcjet Engine Performance: Experiment and Theory,"
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levels available from typically used arcjet engines are very low compared with chemical engines.
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NASA Technical note TN D-2868, NASA Lewis Research Center, June 1965 (accessed September 8 2014)
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satellites using hydrazine as a propellant, providing over 585 s average
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30 Years of Electric Propulsion Flight Experience at Aerojet Rocketdyne
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Institute of Space Systems at the University of Stuttgart
844: 823: 767: 714: 705: 670: 624: 593: 555: 546: 516: 485: 442: 416: 409: 346: 281: 47:) is created in a flow of propellant (typically 259: 8: 73:series arcjet engines are currently used on 239:Aerojet Rocketdyne - Arcjet thruster vendor 711: 552: 413: 266: 252: 244: 130:http://arc.aiaa.org/doi/pdf/10.2514/3.2103 37:electrically powered spacecraft propulsion 140:Wallner, Lewis E. and Czika, Joseph, Jr, 678:Atmosphere-breathing electric propulsion 218:Lichtbogenantriebe für Weltraumaufgaben 117: 143:ARC-Jet Thrustor for Space Propulsion 7: 583:Field-emission electric propulsion 25: 657:Microwave electrothermal thruster 929: 196:Bietigheim-Bissingen, 11/20/2008 787:Pulsed nuclear thermal rocket‎ 683:High Power Electric Propulsion 1: 642:Helicon double-layer thruster 611:Electrodeless plasma thruster 606:Magnetoplasmadynamic thruster 227:Arcjet (Lichtbogentriebwerk) 972: 927: 601:Pulsed inductive thruster 775:Nuclear pulse propulsion 534:Electric-pump-fed engine 434:Hybrid-propellant rocket 424:Liquid-propellant rocket 831:Beam-powered propulsion 804:Fission-fragment rocket 759:Nuclear photonic rocket 727:Nuclear electric rocket 493:Staged combustion cycle 429:Solid-propellant rocket 201:March 18, 2014, at the 106:polytetrafluoroethylene 94:University of Stuttgart 882:Non-rocket spacelaunch 732:Nuclear thermal rocket 632:Pulsed plasma thruster 64:monopropellant rockets 548:Electrical propulsion 275:Spacecraft propulsion 126:AIAA Journal, Vol. 1, 92:, researchers at the 75:Lockheed Martin A2100 780:Antimatter-catalyzed 578:Hall-effect thruster 391:Solar thermal rocket 41:electrical discharge 722:Direct Fusion Drive 637:Vacuum arc thruster 524:Pressure-fed engine 503:Gas-generator cycle 410:Chemical propulsion 347:Physical propulsion 128:No. 11, Nov. 1963. 108:(PTFE) propellant. 102:Baden-Württemberg 1 936:Spaceflight portal 902:Reactionless drive 867:Aerogravity assist 707:Nuclear propulsion 956:Rocket propulsion 943: 942: 897:Atmospheric entry 852:Orbital mechanics 819: 818: 701: 700: 652:Resistojet rocket 542: 541: 517:Intake mechanisms 450:Liquid propellant 354:Cold gas thruster 16:(Redirected from 963: 933: 917:Alcubierre drive 907:Field propulsion 857:Orbital maneuver 845:Related concepts 712: 563:Colloid thruster 553: 414: 316:Specific impulse 268: 261: 254: 245: 205: 193: 187: 186: 179: 173: 172: 170: 168: 154: 148: 138: 132: 122: 79:specific impulse 21: 971: 970: 966: 965: 964: 962: 961: 960: 946: 945: 944: 939: 923: 840: 815: 763: 697: 666: 620: 594:Electromagnetic 589: 538: 529:Pump-fed engine 512: 481: 438: 405: 342: 333:Rocket equation 299:Reaction engine 277: 272: 235: 214: 212:Further reading 209: 208: 203:Wayback Machine 194: 190: 181: 180: 176: 166: 164: 156: 155: 151: 139: 135: 123: 119: 114: 33:arcjet thruster 23: 22: 15: 12: 11: 5: 969: 967: 959: 958: 948: 947: 941: 940: 928: 925: 924: 922: 921: 920: 919: 914: 904: 899: 894: 889: 884: 879: 874: 869: 864: 862:Gravity assist 859: 854: 848: 846: 842: 841: 839: 838: 833: 827: 825: 824:External power 821: 820: 817: 816: 814: 813: 812: 811: 801: 800: 799: 797:Bussard ramjet 789: 784: 783: 782: 771: 769: 765: 764: 762: 761: 756: 755: 754: 749: 744: 739: 729: 724: 718: 716: 709: 703: 702: 699: 698: 696: 695: 690: 685: 680: 674: 672: 668: 667: 665: 664: 659: 654: 649: 644: 639: 634: 628: 626: 625:Electrothermal 622: 621: 619: 618: 613: 608: 603: 597: 595: 591: 590: 588: 587: 586: 585: 580: 575: 565: 559: 557: 550: 544: 543: 540: 539: 537: 536: 531: 526: 520: 518: 514: 513: 511: 510: 505: 500: 498:Expander cycle 495: 489: 487: 483: 482: 480: 479: 474: 469: 467:Monopropellant 464: 463: 462: 457: 446: 444: 440: 439: 437: 436: 431: 426: 420: 418: 411: 407: 406: 404: 403: 398: 393: 388: 383: 378: 377: 376: 366: 361: 356: 350: 348: 344: 343: 341: 340: 338:Thermal rocket 335: 330: 325: 324: 323: 318: 308: 307: 306: 301: 291: 285: 283: 279: 278: 273: 271: 270: 263: 256: 248: 242: 241: 234: 233:External links 231: 230: 229: 224: 213: 210: 207: 206: 188: 174: 149: 133: 116: 115: 113: 110: 39:, in which an 24: 14: 13: 10: 9: 6: 4: 3: 2: 968: 957: 954: 953: 951: 938: 937: 932: 926: 918: 915: 913: 910: 909: 908: 905: 903: 900: 898: 895: 893: 890: 888: 885: 883: 880: 878: 875: 873: 872:Oberth effect 870: 868: 865: 863: 860: 858: 855: 853: 850: 849: 847: 843: 837: 834: 832: 829: 828: 826: 822: 810: 807: 806: 805: 802: 798: 795: 794: 793: 792:Fusion rocket 790: 788: 785: 781: 778: 777: 776: 773: 772: 770: 766: 760: 757: 753: 750: 748: 745: 743: 740: 738: 735: 734: 733: 730: 728: 725: 723: 720: 719: 717: 715:Closed system 713: 710: 708: 704: 694: 691: 689: 686: 684: 681: 679: 676: 675: 673: 669: 663: 660: 658: 655: 653: 650: 648: 647:Arcjet rocket 645: 643: 640: 638: 635: 633: 630: 629: 627: 623: 617: 616:Plasma magnet 614: 612: 609: 607: 604: 602: 599: 598: 596: 592: 584: 581: 579: 576: 574: 571: 570: 569: 566: 564: 561: 560: 558: 556:Electrostatic 554: 551: 549: 545: 535: 532: 530: 527: 525: 522: 521: 519: 515: 509: 508:Tap-off cycle 506: 504: 501: 499: 496: 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Retrieved 161: 152: 141: 136: 125: 120: 87: 68: 61: 32: 28: 26: 892:Aerocapture 887:Aerobraking 768:Open system 752:"Lightbulb" 693:Mass driver 443:Propellants 374:Diffractive 912:Warp drive 742:Salt-water 460:Hypergolic 369:Solar sail 112:References 455:Cryogenic 167:13 August 49:hydrazine 950:Category 747:Gas core 282:Concepts 199:Archived 98:hydrogen 69:Aerojet 836:Tethers 688:MagBeam 573:Gridded 328:Staging 321:Delta-v 90:Germany 53:ammonia 662:VASIMR 311:Thrust 289:Rocket 162:Nasdaq 71:MR-510 57:thrust 18:Arcjet 671:Other 417:State 81:at 2 401:WINE 169:2015 88:In 51:or 45:arc 31:or 27:An 952:: 160:. 85:. 83:kW 66:. 267:e 260:t 253:v 171:. 145:, 43:( 20:)

Index

Arcjet
electrically powered spacecraft propulsion
electrical discharge
arc
hydrazine
ammonia
thrust
monopropellant rockets
MR-510
Lockheed Martin A2100
specific impulse
kW
Germany
University of Stuttgart
hydrogen
Baden-Württemberg 1
polytetrafluoroethylene
http://arc.aiaa.org/doi/pdf/10.2514/3.2103
ARC-Jet Thrustor for Space Propulsion
"Lockheed Martin Awards Aerojet Rocketdyne Contract to Provide Propulsion Subsystems on A2100 Satellites"
Bietigheim-Bissingen, 11/20/2008
Archived
Wayback Machine
Institute of Space Systems at the University of Stuttgart
Arcjet (Lichtbogentriebwerk)
Aerojet Rocketdyne - Arcjet thruster vendor
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Spacecraft propulsion

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