1 00:00:35,010 --> 00:00:31,560 low thrust propulsion is essential for 2 00:00:37,110 --> 00:00:35,020 all space missions and NASA's Lewis 3 00:00:39,750 --> 00:00:37,120 research center is conducting programs 4 00:00:42,720 --> 00:00:39,760 to provide a broad range of low thrust 5 00:00:46,650 --> 00:00:42,730 propulsion concepts for these auxiliary 6 00:00:49,229 --> 00:00:46,660 and primary functions auxiliary 7 00:00:51,630 --> 00:00:49,239 propulsion basically is used for keeping 8 00:00:57,200 --> 00:00:51,640 space systems in desired locations or 9 00:01:00,060 --> 00:00:57,210 for orientation typical examples are the 10 00:01:03,900 --> 00:01:00,070 reaction control systems for earth to 11 00:01:07,050 --> 00:01:03,910 orbit vehicles drag makeup and attitude 12 00:01:10,410 --> 00:01:07,060 control for low Earth orbit systems such 13 00:01:13,230 --> 00:01:10,420 as the Space Station freedom station 14 00:01:17,190 --> 00:01:13,240 keeping for higher orbit systems such as 15 00:01:21,240 --> 00:01:17,200 geosynchronous satellites and then retro 16 00:01:23,490 --> 00:01:21,250 functions near planetary bodies primary 17 00:01:26,039 --> 00:01:23,500 propulsion functions include the moving 18 00:01:29,340 --> 00:01:26,049 of space vehicles from point to point in 19 00:01:32,300 --> 00:01:29,350 earth space as well as propulsion from 20 00:01:36,539 --> 00:01:32,310 Earth space to various planetary bodies 21 00:01:39,450 --> 00:01:36,549 on earth to orbit vehicles such as the 22 00:01:41,100 --> 00:01:39,460 Shuttle Orbiter low thrust propulsion 23 00:01:44,429 --> 00:01:41,110 systems are used to control the 24 00:01:46,440 --> 00:01:44,439 orientation of the vehicle examples 25 00:01:49,130 --> 00:01:46,450 would be to control the movement of the 26 00:01:51,810 --> 00:01:49,140 shuttle orbiter to face the Sun or 27 00:01:54,630 --> 00:01:51,820 reorient it to meet other specific 28 00:01:58,080 --> 00:01:54,640 requirements and then to deorbit the 29 00:01:59,730 --> 00:01:58,090 shuttle for its return to Earth the low 30 00:02:02,399 --> 00:01:59,740 thrust devices used for these 31 00:02:05,730 --> 00:02:02,409 applications are called reaction control 32 00:02:09,149 --> 00:02:05,740 systems for use on the space station 33 00:02:11,630 --> 00:02:09,159 freedom to different times of low thrust 34 00:02:15,930 --> 00:02:11,640 propulsion systems have been selected 35 00:02:17,490 --> 00:02:15,940 for drag makeup thrusters call resistol 36 00:02:20,440 --> 00:02:17,500 jets will be 37 00:02:22,570 --> 00:02:20,450 these resistor Jets will use the waste 38 00:02:26,050 --> 00:02:22,580 gas from the various Space Station 39 00:02:28,090 --> 00:02:26,060 modules this approach eliminates the 40 00:02:30,610 --> 00:02:28,100 requirement for the launch of drag 41 00:02:34,720 --> 00:02:30,620 makeup propellant and the return of 42 00:02:37,030 --> 00:02:34,730 waste gases for the attitude control of 43 00:02:40,900 --> 00:02:37,040 the space station lewis is working on 44 00:02:43,390 --> 00:02:40,910 small chemical rockets these engines are 45 00:02:45,610 --> 00:02:43,400 used to control the torques and forces 46 00:02:48,640 --> 00:02:45,620 that are created during shuttle birthing 47 00:02:52,720 --> 00:02:48,650 and other situations where moderate 48 00:02:55,390 --> 00:02:52,730 thrust levels are required high Earth 49 00:02:58,410 --> 00:02:55,400 orbit systems need two very different 50 00:03:01,840 --> 00:02:58,420 kinds of auxiliary propulsion systems 51 00:03:04,930 --> 00:03:01,850 first when geosynchronous satellites are 52 00:03:07,390 --> 00:03:04,940 placed into orbit an apogee propulsion 53 00:03:09,790 --> 00:03:07,400 system is required to circularize the 54 00:03:13,510 --> 00:03:09,800 satellite and place it into the correct 55 00:03:15,130 --> 00:03:13,520 orbit the geosynchronous orbit is the 56 00:03:16,960 --> 00:03:15,140 one that makes the satellite appear to 57 00:03:19,960 --> 00:03:16,970 be in a fixed position when viewed from 58 00:03:23,080 --> 00:03:19,970 the earth in order to keep the 59 00:03:25,690 --> 00:03:23,090 satellites in desired orbit NASA Lewis 60 00:03:30,160 --> 00:03:25,700 is working on very low thrust Electric 61 00:03:32,770 --> 00:03:30,170 Rockets called arc Jets a final example 62 00:03:35,650 --> 00:03:32,780 of auxiliary propulsion is the use of 63 00:03:38,770 --> 00:03:35,660 chemical rockets near planetary bodies 64 00:03:41,170 --> 00:03:38,780 it is necessary to provide a retro 65 00:03:43,930 --> 00:03:41,180 propulsion maneuver at planetary bodies 66 00:03:46,180 --> 00:03:43,940 so they may be captured and allow the 67 00:03:49,690 --> 00:03:46,190 spacecraft to go into orbit around the 68 00:03:54,009 --> 00:03:49,700 bodies or simply to slow down to obtain 69 00:03:56,199 --> 00:03:54,019 desired data primary propulsion is being 70 00:03:59,979 --> 00:03:56,209 developed for use in both Earth orbit 71 00:04:02,229 --> 00:03:59,989 and for planetary missions planetary 72 00:04:05,350 --> 00:04:02,239 missions include the transfer of systems 73 00:04:10,600 --> 00:04:05,360 to beyond Earth space to such targets as 74 00:04:13,630 --> 00:04:10,610 planets comets and asteroids in summary 75 00:04:17,770 --> 00:04:13,640 then all space missions use low thrust 76 00:04:19,870 --> 00:04:17,780 propulsion in one form or another the 77 00:04:22,870 --> 00:04:19,880 Lewis research center is conducting a 78 00:04:26,380 --> 00:04:22,880 low thrust propulsion program utilizing 79 00:04:27,480 --> 00:04:26,390 an in-house University and industrial 80 00:04:30,390 --> 00:04:27,490 team 81 00:04:32,939 --> 00:04:30,400 this blend of skill and capability 82 00:04:35,210 --> 00:04:32,949 assure that the program will develop 83 00:04:38,040 --> 00:04:35,220 practical devices for near-term 84 00:04:41,129 --> 00:04:38,050 applications and at the same time 85 00:04:44,700 --> 00:04:41,139 produce more advanced concepts for the