1 00:00:08,810 --> 00:00:07,070 good morning everyone this is our launch 2 00:00:12,020 --> 00:00:08,820 contingency news conference from 3 00:00:13,820 --> 00:00:12,030 Vandenberg Air Force Base and here to 4 00:00:16,070 --> 00:00:13,830 discuss what happened this morning with 5 00:00:19,880 --> 00:00:16,080 our Taurus launch with the glory 6 00:00:23,560 --> 00:00:19,890 spacecraft is Omar Baez the NASA launch 7 00:00:27,200 --> 00:00:23,570 director from the Kennedy Space Center 8 00:00:29,060 --> 00:00:27,210 Ron gray be the general manager for the 9 00:00:32,990 --> 00:00:29,070 orbital sciences corporation launch 10 00:00:34,700 --> 00:00:33,000 systems group rich Straka 11 00:00:36,549 --> 00:00:34,710 the deputy general manager for 12 00:00:40,000 --> 00:00:36,559 operations from the Orbital Sciences 13 00:00:42,950 --> 00:00:40,010 corporations launch systems group and 14 00:00:44,720 --> 00:00:42,960 Mike Luthor the deputy associate 15 00:00:46,310 --> 00:00:44,730 administrator for programs for the 16 00:00:49,250 --> 00:00:46,320 science Mission Directorate at NASA 17 00:00:53,680 --> 00:00:49,260 headquarters and we'll begin first with 18 00:00:56,990 --> 00:00:53,690 Omar Baez Omar thank you George 19 00:00:59,209 --> 00:00:57,000 it's a very difficult situation we're in 20 00:01:04,100 --> 00:00:59,219 here and I'm going to try to explain to 21 00:01:06,010 --> 00:01:04,110 you what happened last night and into 22 00:01:09,500 --> 00:01:06,020 this morning as far as the countdown and 23 00:01:13,730 --> 00:01:09,510 all the events as we got through them 24 00:01:16,940 --> 00:01:13,740 and what we know to this point the last 25 00:01:19,910 --> 00:01:16,950 night our team came in at 10 p.m. to 26 00:01:24,710 --> 00:01:19,920 open up the checklist for the Taurus t9 27 00:01:27,530 --> 00:01:24,720 glory mission we set up the facilities 28 00:01:31,730 --> 00:01:27,540 in a range powered up the Taurus launch 29 00:01:33,649 --> 00:01:31,740 vehicle we checked out the FTS system we 30 00:01:38,950 --> 00:01:33,659 got through our polls we got into the 31 00:01:42,050 --> 00:01:38,960 hot count we encountered no anomalies 32 00:01:46,359 --> 00:01:42,060 with the spacecraft or the launch 33 00:01:54,289 --> 00:01:49,130 at t-minus five minutes we did our last 34 00:01:59,260 --> 00:01:54,299 poll and we lifted off at 209 43 this 35 00:02:04,260 --> 00:02:02,590 state zero burn nominally for a minute 36 00:02:09,100 --> 00:02:04,270 and 25 seconds 37 00:02:11,710 --> 00:02:09,110 stage 1 then ignited in a millisecond 38 00:02:17,170 --> 00:02:11,720 later we separated from the stage zero 39 00:02:21,430 --> 00:02:17,180 and continued from flight we did that 40 00:02:24,729 --> 00:02:21,440 till 2 minutes and 45 seconds where we 41 00:02:30,790 --> 00:02:24,739 had indication of burnout of the stage 1 42 00:02:35,860 --> 00:02:30,800 and we had ignition of stage 2 about 6 43 00:02:39,390 --> 00:02:35,870 seconds later after stage 2 ignition we 44 00:02:42,670 --> 00:02:39,400 were expecting to see the fairing on the 45 00:02:47,500 --> 00:02:42,680 t9 separate we didn't see the indication 46 00:02:49,300 --> 00:02:47,510 of fairing separation there was other 47 00:02:51,310 --> 00:02:49,310 indications such as performance loss 48 00:02:58,800 --> 00:02:51,320 that we saw a little bit later on and 49 00:03:10,539 --> 00:03:03,330 and all indications are that the 50 00:03:15,729 --> 00:03:10,549 satellite in rocket order is in the 51 00:03:18,580 --> 00:03:15,739 Southern Pacific Ocean somewhere and 52 00:03:19,300 --> 00:03:18,590 that's all I have for you all right 53 00:03:22,390 --> 00:03:19,310 Thank You Omar 54 00:03:24,220 --> 00:03:22,400 and now to ron gray be the general 55 00:03:26,729 --> 00:03:24,230 manager for the orbital sciences 56 00:03:30,520 --> 00:03:26,739 corporation loft Systems Group rod 57 00:03:34,229 --> 00:03:30,530 thanks well let me just say this is a 58 00:03:36,759 --> 00:03:34,239 pretty tough night for all of us a 59 00:03:39,280 --> 00:03:36,769 little over two years ago we had a 60 00:03:43,060 --> 00:03:39,290 similar tough night when we conducted a 61 00:03:46,289 --> 00:03:43,070 Taurus launch for the OC o mission that 62 00:03:49,150 --> 00:03:46,299 mission suffered a failure the failure 63 00:03:53,819 --> 00:03:49,160 was a failure of the fairing to to 64 00:03:57,069 --> 00:03:53,829 separate we conducted an extensive 65 00:03:59,740 --> 00:03:57,079 investigation of that anomaly and we 66 00:04:01,150 --> 00:03:59,750 traced the most probable cause to a 67 00:04:05,710 --> 00:04:01,160 failure of the fairing separation 68 00:04:08,949 --> 00:04:05,720 initiation system we spent the last two 69 00:04:10,870 --> 00:04:08,959 years doing the analysis on what went 70 00:04:14,120 --> 00:04:10,880 wrong the last 71 00:04:18,320 --> 00:04:14,130 redesigning the system and testing the 72 00:04:20,120 --> 00:04:18,330 components of the system we went so far 73 00:04:23,690 --> 00:04:20,130 as to completely change out the 74 00:04:25,400 --> 00:04:23,700 initiation system to a system that we 75 00:04:28,970 --> 00:04:25,410 use on one of our other vehicles the 76 00:04:31,220 --> 00:04:28,980 Minotaur for vehicle and in the 77 00:04:35,750 --> 00:04:31,230 intervening two years that that system 78 00:04:37,640 --> 00:04:35,760 has flown successfully three times so we 79 00:04:39,680 --> 00:04:37,650 really went into this flight feeling 80 00:04:42,830 --> 00:04:39,690 confident that we had nailed the fairing 81 00:04:47,920 --> 00:04:42,840 issue and then we came up with the 82 00:04:55,160 --> 00:04:51,950 let me just say that there's a great 83 00:04:58,570 --> 00:04:55,170 deal of emotional investment on the part 84 00:05:01,340 --> 00:04:58,580 of all the players on any spaceflight 85 00:05:05,290 --> 00:05:01,350 but that's probably doubly so on a 86 00:05:08,780 --> 00:05:05,300 return to flight effort like this one 87 00:05:10,610 --> 00:05:08,790 I'll just speak briefly to the you know 88 00:05:12,680 --> 00:05:10,620 this is the emotional state if you will 89 00:05:15,410 --> 00:05:12,690 of the of the team and I mean the broad 90 00:05:18,740 --> 00:05:15,420 team the launch team the spacecraft team 91 00:05:20,480 --> 00:05:18,750 on both the industry and the NASA side I 92 00:05:22,220 --> 00:05:20,490 would I think it's not an understatement 93 00:05:27,770 --> 00:05:22,230 to say that tonight we're all pretty 94 00:05:29,180 --> 00:05:27,780 devastated but we will recover well but 95 00:05:32,540 --> 00:05:29,190 the team will bounce back because 96 00:05:34,040 --> 00:05:32,550 they're all professionals and orbital 97 00:05:38,030 --> 00:05:34,050 sciences will bounce back with the 98 00:05:40,270 --> 00:05:38,040 Taurus vehicle let me turn it over to 99 00:05:42,680 --> 00:05:40,280 rich Straka and rich will go through 100 00:05:44,630 --> 00:05:42,690 some of the differences between the 101 00:05:46,790 --> 00:05:44,640 system that we flew on Osio and what we 102 00:05:48,890 --> 00:05:46,800 flew here tonight all right thank you 103 00:05:50,870 --> 00:05:48,900 rod and which track has the deputy 104 00:05:53,410 --> 00:05:50,880 general manager for operations for 105 00:05:56,390 --> 00:05:53,420 orbital sciences long Systems Group rich 106 00:05:58,040 --> 00:05:56,400 okay to give you an idea of what we 107 00:05:59,750 --> 00:05:58,050 changed I'll just go through a brief 108 00:06:02,570 --> 00:05:59,760 description of how that what the fairing 109 00:06:05,210 --> 00:06:02,580 is and how it works the Taurus uses a 110 00:06:07,040 --> 00:06:05,220 clamshell fairing and the fairing is 111 00:06:09,170 --> 00:06:07,050 held onto the vehicle we're constrained 112 00:06:12,320 --> 00:06:09,180 the vehicle with what we call frangible 113 00:06:14,690 --> 00:06:12,330 joints and those joints are meant to 114 00:06:18,020 --> 00:06:14,700 explosively fracture when commanded to 115 00:06:19,830 --> 00:06:18,030 do so when the joints explosively 116 00:06:23,730 --> 00:06:19,840 fracture 117 00:06:26,040 --> 00:06:23,740 the fairing is then in two halves and 118 00:06:30,600 --> 00:06:26,050 there are piston pushers that push the 119 00:06:33,570 --> 00:06:30,610 fairing off in the OCO vehicle and 120 00:06:35,820 --> 00:06:33,580 previous tourist vehicles we use what 121 00:06:39,390 --> 00:06:35,830 was called a hot gas system to do that 122 00:06:42,210 --> 00:06:39,400 pushing job so there was a pyro 123 00:06:45,270 --> 00:06:42,220 technically initiated combustion process 124 00:06:48,030 --> 00:06:45,280 that generated hot gas and the pressure 125 00:06:50,970 --> 00:06:48,040 of that hot gas pushing the Pistons 126 00:06:54,920 --> 00:06:50,980 pushed the fairing halves apart 127 00:06:57,480 --> 00:06:54,930 as Ron said in the investigation we 128 00:07:01,320 --> 00:06:57,490 identified the most probable cause of 129 00:07:05,760 --> 00:07:01,330 the OCO failure as a failure to initiate 130 00:07:08,220 --> 00:07:05,770 that hot gas combustion process so what 131 00:07:10,320 --> 00:07:08,230 we did in response to that is we swapped 132 00:07:13,080 --> 00:07:10,330 out or we changed out redesigned the 133 00:07:16,350 --> 00:07:13,090 deployment system to use a cold gas 134 00:07:19,940 --> 00:07:16,360 system which is a pressurized bottle of 135 00:07:22,470 --> 00:07:19,950 nitrogen that then when commanded 136 00:07:24,360 --> 00:07:22,480 functions by pressurizing those same 137 00:07:28,050 --> 00:07:24,370 Pistons and pushing the fairing halves 138 00:07:29,909 --> 00:07:28,060 apart it uses a completely different a 139 00:07:32,400 --> 00:07:29,919 Nisshin system and a completely 140 00:07:35,340 --> 00:07:32,410 different pressurization methodology 141 00:07:37,409 --> 00:07:35,350 than the OCO system and as Ron said we 142 00:07:40,980 --> 00:07:37,419 we really felt like we had the problem 143 00:07:44,130 --> 00:07:40,990 nailed and that particular system has 144 00:07:46,770 --> 00:07:44,140 flown three times last year a very 145 00:07:48,900 --> 00:07:46,780 similar system almost identical system 146 00:07:54,140 --> 00:07:48,910 flew and our Minotaur four product lines 147 00:07:58,230 --> 00:07:54,150 successfully three times last year so 148 00:08:00,480 --> 00:07:58,240 right now we're crunching the data but 149 00:08:02,370 --> 00:08:00,490 there was really not enough data that's 150 00:08:05,460 --> 00:08:02,380 been processed so far to really tell any 151 00:08:08,340 --> 00:08:05,470 more than the fairing didn't didn't 152 00:08:11,760 --> 00:08:08,350 deploy and that's about all I have to 153 00:08:13,409 --> 00:08:11,770 say thank you rich and Mike Luthor the 154 00:08:15,090 --> 00:08:13,419 deputy associate administrator for 155 00:08:16,680 --> 00:08:15,100 ministration for programs for the 156 00:08:20,550 --> 00:08:16,690 science Mission Directorate and NASA 157 00:08:21,930 --> 00:08:20,560 headquarters Mike well clearly the 158 00:08:24,300 --> 00:08:21,940 science Mission Directorate and the 159 00:08:27,690 --> 00:08:24,310 Earth Science Division is extremely 160 00:08:30,149 --> 00:08:27,700 disappointed in the loss tonight we had 161 00:08:32,189 --> 00:08:30,159 worked closely at all levels of 162 00:08:35,430 --> 00:08:32,199 the agency and with our industry 163 00:08:38,069 --> 00:08:35,440 partners to evaluate this risk and we 164 00:08:40,189 --> 00:08:38,079 felt going in that we believed we had an 165 00:08:44,189 --> 00:08:40,199 acceptable level of risk 166 00:08:46,439 --> 00:08:44,199 clearly we missed something so we've now 167 00:08:48,780 --> 00:08:46,449 got to go off find out what that is 168 00:08:54,900 --> 00:08:48,790 fix it and that is in fact what we will 169 00:08:56,400 --> 00:08:54,910 do in the meantime we we have lost the 170 00:08:58,499 --> 00:08:56,410 glory mission it would have made 171 00:09:02,040 --> 00:08:58,509 important measurements for the 172 00:09:04,340 --> 00:09:02,050 understanding of earth as a system and 173 00:09:08,490 --> 00:09:04,350 of the impacts of climate change 174 00:09:09,689 --> 00:09:08,500 however the earth SMD science Mission 175 00:09:12,540 --> 00:09:09,699 Directorate and the Earth Science 176 00:09:15,329 --> 00:09:12,550 Division will continue to contribute and 177 00:09:18,710 --> 00:09:15,339 make significant contributions to the 178 00:09:21,629 --> 00:09:18,720 understanding of the earth with its 13 179 00:09:25,980 --> 00:09:21,639 existing operating missions and a cadre 180 00:09:29,129 --> 00:09:25,990 of aircraft and ground networks and data 181 00:09:32,670 --> 00:09:29,139 systems contributing to our science 182 00:09:35,280 --> 00:09:32,680 research in addition we'll continue to 183 00:09:40,319 --> 00:09:35,290 plan the path forward into the next 184 00:09:41,850 --> 00:09:40,329 decade with a CAD Dre of more than a 185 00:09:45,720 --> 00:09:41,860 dozen missions to be launched in the 186 00:09:47,629 --> 00:09:45,730 next 10 years all right 187 00:09:50,009 --> 00:09:47,639 thank you Mike and we're ready now for 188 00:09:52,079 --> 00:09:50,019 questions please give your name and 189 00:09:53,579 --> 00:09:52,089 affiliation when the microphone comes to 190 00:09:55,740 --> 00:09:53,589 you we'll start in the front with Nora 191 00:09:57,660 --> 00:09:55,750 Thank You Nora Wallace at the Santa 192 00:09:59,579 --> 00:09:57,670 Barbara News Press Omar you said 193 00:10:01,920 --> 00:09:59,589 something about other indications of 194 00:10:06,720 --> 00:10:01,930 performance loss can you expand on that 195 00:10:09,650 --> 00:10:06,730 at all yeah what you see is since we 196 00:10:12,870 --> 00:10:09,660 didn't jettison the fairing you see 197 00:10:16,019 --> 00:10:12,880 we're we're expecting to shed weight as 198 00:10:18,150 --> 00:10:16,029 a fairing comes off and obviously 199 00:10:20,429 --> 00:10:18,160 wouldn't shed that way and the rocket 200 00:10:27,370 --> 00:10:20,439 just can't carry you into orbit with 201 00:10:32,120 --> 00:10:29,810 Janine's skully santa maria times Lompoc 202 00:10:34,100 --> 00:10:32,130 record can you I know it's still early 203 00:10:36,790 --> 00:10:34,110 and you haven't thoroughly gone through 204 00:10:40,460 --> 00:10:36,800 the data but can someone explain how 205 00:10:42,830 --> 00:10:40,470 similar this is to the OSI Oh failure 206 00:10:46,930 --> 00:10:42,840 do you have indication of partial 207 00:10:49,130 --> 00:10:46,940 separation is there any kind of 208 00:10:53,360 --> 00:10:49,140 assessment that you can give in terms of 209 00:10:55,370 --> 00:10:53,370 Oh coz I guess I can take that we really 210 00:10:57,950 --> 00:10:55,380 don't have any of the data processed yet 211 00:11:00,650 --> 00:10:57,960 it's going to be several hours before we 212 00:11:03,260 --> 00:11:00,660 get a good look at the data so it's too 213 00:11:05,240 --> 00:11:03,270 early to tell whether it's it's the same 214 00:11:08,150 --> 00:11:05,250 thing as we faced last time in terms of 215 00:11:10,000 --> 00:11:08,160 the you know the symptoms and the data 216 00:11:13,130 --> 00:11:10,010 pattern we just don't know right now 217 00:11:15,110 --> 00:11:13,140 what I can say is that we did put 218 00:11:16,670 --> 00:11:15,120 additional telemetry points and we do 219 00:11:21,100 --> 00:11:16,680 have additional instrumentation 220 00:11:25,010 --> 00:11:21,110 on this flight so we do have a leg up on 221 00:11:26,840 --> 00:11:25,020 determining root cause this time and but 222 00:11:31,850 --> 00:11:26,850 it's too early to tell if it if it is in 223 00:11:34,190 --> 00:11:31,860 fact the same cause Omar are you going 224 00:11:37,100 --> 00:11:34,200 to be able to pinpoint more where the 225 00:11:39,890 --> 00:11:37,110 satellite might have ended up yeah like 226 00:11:42,740 --> 00:11:39,900 we should be able to it's just too 227 00:11:45,650 --> 00:11:42,750 preliminary to get the trajectory of 228 00:11:49,850 --> 00:11:45,660 word ended up but seeing that it's 229 00:11:53,030 --> 00:11:49,860 similar weight to what oka was and the 230 00:11:55,460 --> 00:11:53,040 same launch vehicle performance it's 231 00:11:59,320 --> 00:11:55,470 likely physics says it's likely in the 232 00:12:04,790 --> 00:12:02,960 can you explain is there any kind of 233 00:12:08,390 --> 00:12:04,800 difference between the system that's 234 00:12:10,940 --> 00:12:08,400 been used on glory versus what's flown 235 00:12:16,130 --> 00:12:10,950 successfully on Minotaur and in terms of 236 00:12:20,570 --> 00:12:16,140 trying to figure what what happened the 237 00:12:22,610 --> 00:12:20,580 the fairing system itself is is very 238 00:12:26,990 --> 00:12:22,620 similar but they are different fairings 239 00:12:28,760 --> 00:12:27,000 between the two vehicles the there are 240 00:12:31,300 --> 00:12:28,770 different sizes for one thing the 241 00:12:33,590 --> 00:12:31,310 Minotaur fairing is quite a bit larger 242 00:12:35,780 --> 00:12:33,600 but it does use the same basic 243 00:12:38,960 --> 00:12:35,790 mechanisms the same frangible joint 244 00:12:39,380 --> 00:12:38,970 system for for the separation or the 245 00:12:42,380 --> 00:12:39,390 frack 246 00:12:45,100 --> 00:12:42,390 during process and the jettison system 247 00:12:48,650 --> 00:12:45,110 the piston system is is almost identical 248 00:12:52,010 --> 00:12:48,660 so but but there are differences in 249 00:12:58,460 --> 00:12:52,020 terms of the fairing size and and the 250 00:13:01,130 --> 00:12:58,470 geometry of the fairing from NASA 251 00:13:03,830 --> 00:13:01,140 standpoint if you can speak maybe expand 252 00:13:05,390 --> 00:13:03,840 a little bit on how the earth science 253 00:13:07,550 --> 00:13:05,400 group and the scientists here who've 254 00:13:11,090 --> 00:13:07,560 spent decades on this mission rebound 255 00:13:13,370 --> 00:13:11,100 from this and how how the crew might 256 00:13:18,290 --> 00:13:13,380 bond together in this to recover from 257 00:13:21,920 --> 00:13:18,300 this loss well as as as you mentioned 258 00:13:25,280 --> 00:13:21,930 the these missions are developed as you 259 00:13:29,980 --> 00:13:25,290 well know over a course of a number of 260 00:13:34,400 --> 00:13:29,990 years by some very dedicated people 261 00:13:37,730 --> 00:13:34,410 overcoming great odds and develop that 262 00:13:42,260 --> 00:13:37,740 really as a family and and so they 263 00:13:45,230 --> 00:13:42,270 respond to disappointments as a fan as a 264 00:13:49,640 --> 00:13:45,240 family would quite frankly and so I 265 00:13:53,630 --> 00:13:49,650 think you know if you can imagine how 266 00:13:56,450 --> 00:13:53,640 any family responds to a loss that might 267 00:13:57,500 --> 00:13:56,460 occur they've overcome other obstacles 268 00:13:59,270 --> 00:13:57,510 previously 269 00:14:02,840 --> 00:13:59,280 I'm sure they'll overcome this one 270 00:14:04,610 --> 00:14:02,850 although it is quite painful after 271 00:14:11,510 --> 00:14:04,620 having dedicated so many years of your 272 00:14:14,810 --> 00:14:11,520 life can you comment on the status of 273 00:14:18,950 --> 00:14:14,820 co2 will it still use the current plan 274 00:14:20,900 --> 00:14:18,960 is to fly on a Taurus XL is that what's 275 00:14:24,800 --> 00:14:20,910 the plan now 276 00:14:26,870 --> 00:14:24,810 is is in development and a couple of 277 00:14:29,450 --> 00:14:26,880 years away from launch yet we'll have to 278 00:14:32,270 --> 00:14:29,460 evaluate you know the outcome of this 279 00:14:42,860 --> 00:14:32,280 investigation and and we'll adjust our 280 00:14:47,990 --> 00:14:45,200 all right in that event saying millon