Двигательная установка. XIPS-13. [Редактировать]

Технические характеристики

#ХарактеристикаЗначение
1Тяга, мН18
2Удельный импульс, метра в секунду23500
3Мощность, Вт450

Найдено 120 документов по запросу «XIPS-13». [Перейти к поиску]


Дата загрузки: 2017-06-15
Скачать документ
Скачать текст
0.17/5
... ion thruster and the derated XIPS-30 are about tied for... the NH3 arcjet and the XIPS-25 close behind. When these... in scope to either the XIPS-13 or the HAJ, assumed to... to each EPS. The small XIPS is included for NSSK only... of EPS's EPS Device XIPS-13 XIPS-25 XIPS-30 SPT-100 H2AJ H2RJ... GIM PMU STRU HARN MISC XIPS-13 XIPS-25 XIPS-30 SPT-100 H2AJ....0 21.0 21.0 In Table 3, the XIPS-13 and -25 thruster masses include..., are given in parentheses below. 3.0 XIPS-25 Mbol T. mo Mbol 3717...(2647) 2638(2525) 19.8 11.4 6.7 3.9 1.8 XIPS-30 H2 AJ Mbol T. mo... for added redundancy (configuration 2). 3. The XIPS-30 (de-rated) for both... thruster system, and a four thruster XIPS-13 system for NSSK (configuration 4). The... with only 4 thrusters, since the XIPS-30 thruster has been shown... in this example. For the XIPS-30, 4-thruster system, the increase... between it and the 4-thruster XIPS-13 system which would be used... velocity of the XIPS-30 relative to the XIPS-13. The 1869 IEPC... assigned to OR with the XIPS-30 is the sum of... as configuration 1, except that the XIPS-13 ion thrusters are mounted at... in BOL Mass SPT-100 XIPS-30 63 133 198 333...-100 (configuration 2) and the derated XIPS-30 (configuration 3) are also substantial... the SPT-100 and the XIPS-30, the hardware is more... need be added; for the XIPS-30, only the increased cost... thrusters relative to that of 13 cm thrusters need be considered... S 46 a. H2RJ b. SPT-100 c. XIPS-30 d. XIPS-25 5000 5740 57 36... WITH XIPS-30'S. XIPS3 CONFIGURATION 4: OR WITH H2RJ's; NSSK WITH XIPS-13's. FIGURE...



Дата загрузки: 2017-09-24
Скачать документ
Скачать текст
Скачать перевод
Посмотреть билингву
0.21/5
... SNAP SNAPSHOT SPIBS ST4 USAF XIPS 1 Goddard Space Flight Center Hughes... 20, 1964 using a Scout vehicle.3,13 This flight experiment had a 8 cm... in the case of the XIPS-25, a preflight development program that...-clear circuits for the IAPS, XIPS, and NSTAR thrusters. One of... ion engine input power was 0.13 kW, and the thrust was... due to lack of funding. XIPS-25 (4.2 kW) A 25 cm diameter... HS 702 spacecraft use four XIPS-25 engines and two PPUs... HS 702 spacecraft with the XIPS-25. The spacecraft has an... thrust at 3800 s specific impulse. XIPS hardware is currently under extended....2 m long vacuum facility. XIPS-25 (1.3 kW) This XIPS-25 program, conducted by... XIPS-13 (0.44 kW) and XIPS-25 (4.2 kW) systems, instead of the 1.3 kW XIPS... cathodes.64 Ground tests of 13 cm and 30 cm diameter... Hughes' first customer for the XIPS-13 propulsion system on PAS-5. This... spacecraft are operational using the XIPS-13 system namely, Galaxy VIII-i, ASTRA... many communications spacecraft employing the XIPS-13 and XIPS-25 propulsion systems. Additionally... Paper 73-1133, October 1973. 13. Gold, H., et al., "Description and... Electronics, November 1965, pp. 13–B1 to 13–B16. 27. Olsen, O. C., "Investigation... of Spacecraft and Rockets, Vol. 13, No. 2, February 1976, pp. 106...—1999-209439 11 52. Beattie, J. R., "XIPS Keeps Satellites on Track," The.../7 02/702.html. 54. Anon., "XIPS: The Latest Thrust in Propulsion....hughespace.com/factsheets/xi ps/xips.html. 55. Kaufman, H. R., "An Ion... to the S/C systems. Ref. 16 13 Table 1b. Experimental Flights of... SEPST SIT-5 SEPS IAPS XIPS-25 XIPS-25 Sponsor NASA JPL NASA... thruster 2.5 kW 0.072 kW 2.6 kW 0.13 kW 1.3 kW 4.2 kW Maximum t hr... 4 4 4 1 4 4 Thruster diameter 13 cm 13 cm 13 cm 30 cm 13 cm 13 cm Type...-cm thruster (Xe) (INTELSAT/Hughes) 13-cm lab thruster (Xe) (Hughes... -> XIPS-13 for comsat NSSK (Hughes) 1998 -> 1999 -> NASA/TM—1999-209439 XIPS... space S/C 18 >8000 h test of XIPS-13 (Hughes) 8193 h test of the... thruster Extended testing of the XIPS-25 (Hughes) Extended groundtesting of...) 1995 2000 Hughes PAS-5, 500 W XIPS (First of many S/C) 2005 Hughes 701 S/C 4.2 kW XIPS Space Technology 4, 3 NSTAR subsystem IPS... AeroSpace Information, (301) 621–0390. 13. ABSTRACT (Maximum 200 words) The...



Дата загрузки: 2017-09-24
Скачать документ
Скачать текст
0.32/5
... Institute of Aeronautics and Astronautics XIPS: XIPS is a gridded ion thruster system... commercial geosynchronous satellite applications.7 The XIPS system is used for orbit... these functions. XIPS has been flown in two varieties, a 13 cm and 25 cm beam diameter thrusters. The XIPS-13 was used on Boeing 601 bus satellites, the XIPS-25... in this analysis. While the XIPS system is at TRL9 for... space mission environments.8 Qualification of XIPS-25 for NASA deep space... readiness and qualification status of XIPS-25 for this mission would... Electric Propulsion System Characteristics NEXT12,13 NSTAR14 XIPS-259 BPT-400010,15... was accomplished, or for the XIPS-25 case, to achieve similar... strings is increased to 3, at 13.5 kW input power, 96 targets... the specific impulse of the XIPS-25 provides efficient xenon use... system configuration complexity significantly. The XIPS-25 solution was modified to... validated through test and analysis.13, 16-19 A long duration test... are within expectations. The first 13,000 hours of the LDT... 904 687 687 7.5 9.0 6.6 6.6 37% 31% 13% Overall Xenon Margin 35% 35..., T. A. Bond and A.M. King “Performance of XIPS Electric Propulsion in Station Keeping..., D.M., et al., “Qualification of Commercial XIPS Ion Thrusters for NASA Deep...,” AIAA-2007-5212, July 2007. 13 Van Noord, J.L., “Lifetime Assessment of...



Дата загрузки: 2017-09-24
Скачать документ
Скачать текст
0.13/5
... NSTAR system is at TRL9. XIPS: XIPS is a gridded ion thruster system... geosynchronous satellite applications.[Ref. 3] The XIPS system is used for orbit... these functions. XIPS has been flown in two varieties, a 13 cm and 25 cm beam diameter thrusters. The XIPS-13 was used on Hughes (Boeing) 601 bus satellites, the XIPS-25... in this analysis. While the XIPS system is at TRL9 for... space missions.[Ref. 4] Qualification of XIPS-25 for NASA deep space... readiness and qualification status of XIPS-25 for this mission would... Propulsion System Characteristics NEXT NSTAR XIPS-25 BPT-4000 Thrust, mN... was accomplished, or for the XIPS-25 case, to achieve similar... strings is increased to 3, at 13.5 kW input power, 96 targets... the specific impulse of the XIPS-25 provides efficient xenon use... system configuration complexity significantly. The XIPS-25 solution was modified to... are within expectations. The first 13,000 hours of the LDT... 904 687 687 7.5 9.0 6.6 6.6 36% 31% 13% Overall Xenon Margin 35% 35...%. The ∆V contingency is greater than 13%. The current Starshade Spacecraft design..., T. A. Bond and A.M. King “Performance of XIPS Electric Propulsion in Station Keeping..., D.M., et al., “Qualification of Commercial XIPS Ion Thrusters for NASA Deep...,” AIAA-2008-4949, July 2008. 13. Herman, D.A., et al., “Performance Characteristics...



Дата загрузки: 2017-03-09
Скачать документ
Скачать текст
0.04/5
.... The SPT-100/140 and XIPS-13/25 thrusters were considered for..., - k=0.05 – propellant (xenon) margin, - atank=0.13 - tank-to-xenon mass ratio... 3000 1630 1630 Ion thrusters/ XIPS 13 cm 25 cm 18 165... thrusters (SPT) and ion thrusters (XIPS) for investigated transportation are submitted... a rule, at the use of XIPS (with more higher specific impulse... kg 1016 kg SPT and XIPS comparison STAR 2 space platform Consumed... 100 day the use of XIPS-25 allows to insert a space... GEO, kg 900 SPT-100 XIPS-13 850 800 750 700 650... Fig. 11. SPT-100 and XIPS-13 comparison In a Fig. 11 mass... to XIPS-13. It is visible, that at the use of XIPS-13 injected... 120 day the use of XIPS-13 allows to insert a space vehicle..., the lower curve corresponds to XIPS-25 using. It is visible, that at the use of XIPS-25 injected mass is SC...., V=7475 m/s) 2000 SPT-140 1900 XIPS-25 1800 1700 1600 1500... Fig. 12. SPT-140 and XIPS-25 comparison 9 • space system Soyuz... space platforms. The using of XIPS results in increase of the... from SPT-100 to the XIPS-13 increases the transfer duration from...



Дата загрузки: 2017-03-09
Скачать документ
Скачать текст
Скачать перевод
Посмотреть билингву
0.06/5
... for change Issue Date Creation 1 13/12/2014 Review 1 1.1 16/12... Hollow Cathode and neutraliser ........................................................................................................................... 25 6.13 Other ...................................................................................................................................................................... 26 EP SUBSYSTEM COMPONENTS... of the different TRL Page 13/73 D1.2 Deliverable Report Date... engine 3000 - 4500 1000 5000 >13.8 Qualification in progress: HPEPS for...-20kWs). Also includes heaterless ignition. 6.13 Laboratory model status. Engineering model... V Airbus DS (Germany) GOCE MPE 13 kV GOCE IBCV 4 * 5 kW 10... for ESA ARTEMIS Microscope PPCU 13 kV 70 W Full power processing... Microscope mission Lisa Pathfinder PCU 13 kV 76 W Full power processing...-cycle heat engine, and SNAP-13 used caesium vapour diodes for...-3 Meteorological satellite SNAP-19B. 2 x 25W 13.5 1.9 5.4 1969 1972 Apollo 12,14... (Navy Navigation) Transit RTG. 35W 13.5 2.6 4.2 1972 1973 Pioneer 10 & 11...-19. 4 per spacecraft @ 40W each 13.6 2.9 5.4 1975 Viking 1 & 2 Mars Lander SNAP-19. 2 per lander @ 42W each 13.6 3.1 5.4 1976 Lincoln LES 8 and LES... – USA XIPS-13 GIE Fly on Boeing 601HP platforms Boeing - USA XIPS-25... developing in the US a 8 cm XIPS ion thruster with the following... manoeuvres. Boeing use the XIPS- 13 and XIPS-25 built by the US... and 702HP platforms respectively. The XIPS-25 (Xenon Ion Propulsion System... Power (W) Thrust (mN) Specific Impulse (s) XIPS-25 22004500 79-165 3400... 35-145 (230 demonstrated) 4400 XIPS-13 421 17.8 2585 TRL9 T5... NEXT 5006900 236 (max) 4190 XIPS-8 100-350 2-14 2000-3000...



Дата загрузки: 2017-09-24
Скачать документ
Скачать текст
0.24/5
...,6 the Xenon Ion Propulsion System (XIPS-13)7 is being marketed and deployed... on a regular basis, and the XIPS-25 system 8 is coming on... led to the NSTAR and XIPS thrusters rather than being an... radio frequency (rf) design,12,13 in which electrons are accelerated... and the 25-cm-diam XIPS-25. 8 The data of Table... SERT I SERT II XIPS-13 1964 1970 1997 10 15 13 Table 2 Propellant... diameter, cm SEPS IAPS NSTAR XIPS-25 1981 1983 1998 1998... Paper 72-474, April 1972. 13 Bassner, H., Bond, R. A., Thompson, V. K., and Groh...



Дата загрузки: 2017-09-24
Скачать документ
Скачать текст
0.2/5
... . . . . . . . . . . . . . . 1.2.4 SMART-1 Mission . . . . . . . . . 1.3 Motivation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 3 6 7 7 9 10 11 13 14 14 15 16 Chapter... [9] b) from [60] . . . . . 3.10 3.11 3.12 3.13 xiii 46 47 48 50... subtracted (vertical polarization). . . . 114 xv 5.13 Comparison of the simulation result... experimental spacecraft. Several ion thrusters (XIPS-13, XIPS-25, IES, and UK-10... XIPS-13 ion thruster on HS601, PAS-5, and Galaxt 8-i satellites and their XIPS... thrusters are listed in Table 1.2. 13 Table 1.2: SPT specifications SPT-35a... x = rc sin(ωc t + φ0 ) + (x0 − rc sinφ0 ) (2.13) y = rc cos(ωc t + φ0 ) + (x0 − rc cos... given by (2.10)-(2.12), and (2.13)-(2.15) for a uniform magnetic field...), (2.11) and (2.12) and from (2.13), (2.14) and (2.15) with q = −e and...] and is shown in Figure 3.13. 57 a) [9] b [21] c) reconstructed Figure 3.12: Electron temperature distributions. a) b) Figure 3.13: Electron temperature distribution a) from [9] b) from... function and is equivalent to 2/ π (3.13) x −t2 e dt. 0 The inversion of (3.13) is given by F −1 (ξ) = √ 2 erf−1 (2ξ − 1) 63 (3....-Boltzmann distribution in many cases [13, 17, 21]. In this numerical... in papers are slightly different [13, 14, 22, 23, 87]. In... experimental data. Figures 5.12 and 5.13 show the comparison between the... background noise. Comparing Figure 5.10-5.13 shows that subtracting the background... 0 3 4 10 10 Frequency (MHz) Figure 5.13: Comparison of the simulation result... shown in Figures 5.12 and 5.13 is used in this comparison... shown in Figures 5.12 and 5.13 is used in this comparison... ak are given by ak = 1 X(kΩ0 ) N (A.13) where Ω0 is the sample spacing... envelope function. Combining (A.9) 168 and (A.13) and replacing x˜[n] by x[n] yield N/2 x[n] = k=−N/2 1 X(kΩ0 )ejk.... Fusion, 42:B323–B339, 2000. [13] J. P. Bouef and L. Garigues. Low frequency... Russia. News from Moscow, (26):9–13, 2000. [69] A. I. Morozov Y. V. Esipchuk G. N. Tilinin...



Дата загрузки: 2017-04-09
Скачать документ
Скачать текст
0.07/5
... 1.45 MN-s per thruster.12,13 In the MR-510 configuration... with an L-3 Communications (then Hughes) XIPS-13 ion engine system. Then, in... BPT4000 (XR-5) system joins the XIPS-25 ion engine system as... Ion Propulsion System, the XIPS-13. The first XIPS system flew on PanAmSat... Exhibit, AIAA 1999-2272, 1999. 13 Zube, D. M. and Cohen, D., “Improvements to....org/assets/documents/nwgs/UCS_Satellite_Database_9-1-13.xls Captured September 21, 2013...



Дата загрузки: 2017-09-24
Скачать документ
Скачать текст
Скачать перевод
Посмотреть билингву
0.29/5
... 10 years lifetime and after 13 years of service it is... power up to 2.5 kW (NSTAR, XIPS 13 cm, T5, RIT 10 cm... satellites with a total of 56 XIPS 25-cm thrusters (4.5 kW ion... Conference, Huntsville Alabama, 2003 5 J. R. Beattie, “XIPS Keeps Satellites on Track”, The..., T. A. Bond and A. M. King “Performance of XIPS Electric Propulsion in Station Keeping... J. S. Snyder, “Performance Evaluation of the XIPS 25-cm Thruster for Application...