Tuesday, July 28, 2015

Prisma

 2010-028B


SSC mission for robotic rendezvous. 140 kg chaser satellite and 40 kg target.

Launch to 700 km x 98.2 deg.

Launch by Dnepr; remain together for initial checkout, then separate later. Control from SSC/Solna via Esrange station.

Prisma Main, Prisma Target - Mango and Tango. SSC is prime contractor with structure by Saab. Main is box + 2 panels; 140 kg wet. size 0.80 x 0.83 x 1.30m. AOCS has 6 x 1N thrusters and 11 kg of hydrazine.

Also carries a 'green' propulsion system. HPGP is High Performance Green Propellant, LMP-103S, with an Isp around 250s. 5 kg of HPGP are connected to 2 x 1N thrusters.


Prisma 
 

DateTimeEventOrbit  

2010 Jun 15 1442 Launch by Dnepr  Yasny 
 1443 T+1:50 Stage 1 sep 
 1447? GO sep
 1448? T+5:54? St 2 sep 
 1448? T+5:55? DU on 
 1458? Plume shield sep 
 1458  Prisma sep  726 x 749 x 98.3 
  Platform A sep 
 1459  Picard sep  693 x 728 x 98.3 
  DS orbit  714 x 1267 x 98.2 
2010 Aug 11  1751  Tango sep 
2010 Aug 20   HPGP tests at 600m range to Tango 
2010 Aug 21   HPGP pulse tests at 1 km range to Tango 
2010 Aug 24   MEMS microthruster tests, partial success 
2010 Aug 26   Range 2.5 km  
2010 Aug 27   Reduce range to 500m 
2010 Aug 30   Begin AFF Early Harvest, range 10 km to 18m 
  Activate FFRF system, range 740 m 
 
2010 Sep 1   Approach from 800 m to 500m? 
2010 Sep 1   Move away toward 5 km 
2010 Sep 2  1200? Stationkeep at 5 km 
 2100 Resume retreat 
2010 Sep 3  1400? Skeep at 10 km  
2010 Sep 3  2300? Resume approach 
2010 Sep 4  1500? Stationkeep at 5 km 
2010 Sep 10   Approach to 150m 
  Approach to 50m 
2010 Sep 14 1950  Range 18m in AFF9 
 2000  Retreating 
2010 Sep 14   Complete AFF-EH 
2010 Sep 16   FFRF initialization at 2 km? 
2010 Sep 16?  Safemode at 9 km  
2010 Sep 17  0500? retreat to safe orbit 
 1512  Safemode exit 
 1651  Set up for FFRF experiment 
 1830  Restored correct orbit at 6 km  
2010 Sep 18   End FFRF-I at 80m 
2010 Sep 20 1820 AFC experiment (DLR)  
  Move to new orbit at 500 x 800 x 400 m, 2 km down track 
2010 Sep 21  1820  AFC to open loop 
2010 Sep 23  1755  AFC to closed-loop at 1881 m mean sep 
2010 Sep 25   AFC rendezvous - relocate to 0m mean sep in 400m ellipse 
  Min distance 150m 
2010 Oct 6   Complete AFC 
2010 Oct 7  FFRF envelope 
  Mango move to 100m behind Tango 
2010 Oct   Ranges from 20m to 9 km  
2010 Oct 13   Complete FFRF envelope part 1 
2010 Oct 18  2000 10m prox ops 
2010 Oct 20   Range 20 m 
2010 Oct 20   T+0 Mango Rendezvous and prox ops - approach from 20m 
  Pass Tango at 7 m  
  T+0:40 Back at 20m 
2010 Oct 26   Flyaround at 10m, 3 relative orbits 
2010 Oct 28   CNES-mode experiments 
2010 Oct 30   Stationkeep at 100m 
2010 Oct 31   Stationkeep at 70m 
2010 Oct 31   Collision avoidance 
2010 Nov 9   HPGP 2 
2010 Dec 7   HPGP 3 propulsion tests 
2011 Jan 25   Prox GPS epxeriments to 2 m 
2011 Feb 12   FFIORD experiments 
2011 Mar 13   FFIORD GNC experiment completed, 80 and 20m 
2011 Apr   ARV 3 continues 
2011 Jul 15  Tango in hibernation 
2011 Jul 18   Mango begin AOK experiment - autonomous orbit control 
2011 Aug   End of nominal mission 
2011 Oct   Extended mission FFIORD 
2011 Nov   Complete extended mission 
2012 Mar 22    99.92 723 x 786 x 98.3 
2012 Apr 23  DLR ARGON experiment 
2012 Apr 27   ARGON complete 
2013 Apr   IRIDES mission - rendezvous with Picard 
2013 May 10    99.90 723 x 784 x 98.3 
2013 May 13  DV Transfer orbit to Picard 
2013 Jun 14    99.90 722 x 785 x 98.3 
2013 Jun 15    99.46 684 x 780 x 98.3 
2013 Jun 20  DV for transfer orbit complete 
2013 Jul 28    98.97 648 x 770 x 98.5 
2014 May 21    98.9 650 x 766 x 98.5 
2014 May 24   Peri raise 
  Orbit plane drift stop, 7 m/s 
2014 Jun 18    98.94 655 x 761 x 98.5 
2014 Jul 14    98.94 655 x 760 x 98.5 
2014 Jul 20   Orbit adjust  98.99 664 x 756 x 98.4 
2014 Aug   Problem with propulsion 
2014 Aug  Rendezvous aborted, flyby 
2014 Sep 17    98.987 668 x 751 x 98.4 
  Orbit tweak? 
2014 Sep 19    98.973 668 x 750 x 98.4 
2014 Sep 24   Orbit tweak, retired? 
2015 Mar 18    98.95 668 x 749 x 98.4 

Payload:

  • FFRF Formation Flying RF sensor, metrology formation flying package, (CNES/Alcatel Alenia/)

  • VBS Vision Based Sensor (DTU/) Optical tracking/prox ops system using star trackers

  • GPS GPS Nav and SAFE (Spaceborner Autonomous Formation Flying Experiment) (DLR/)

  • HPGP High Performance Green Propellant, ADN (ammonium dinitramide) propulsion test, 2 x 1N

  • Steady stream N2 microthruster experiment

Progress M-13M

 2011-062A


Mission 45P, spacecraft 413. Launch mass 7282 kg, 6925 kg at docking, 4328 kg at undocking. Carried 880 kg of prop, 2398 kg of cargo (1350 in GO and 1048 liquids). Carried the Chibis-M satellite in a container; 22 kg satellite plus container 47 kg, although other sources give 34 kg.


M-13M 
 

DateTimeEventOrbit  

2011 Oct 30  1011:12  Launch by Soyuz-U KB LC-1 
 1019  Blok I MECO 
 1020:01  Blok I sep 
 1357:16  DV1 49.6s 19.5m/s 
 1444:49  DV2 30.7s 12.0 m/s 
2011 Nov 1  1112:46  DV3 DPO burn 47s 3.2m/s 
2011 Nov 2  Rendezvous with ISS 
 0920? DV4 SKD burn 31.6m/s 
 1003  DPO correction burn 
 1029  DV 30.3 m/s 
 1107  DV 5.9m/s 
 1113  Braking 
 1115  Braking 
 1122  200m range 
 1129  Stationkeeping 
 1141:33  Docked with Pirs 
2012 Jan 23  2209:34  Undocked from Pirs 
2012 Jan 24  0035  DV 
 0132 DV 
2012 Jan 24  2318:30  Chibis-M sep 
2012 Jan 25  0225:00  Deorbit 235s burn 3:56 125m/s  56? x 514 x 51.6 
 0304  Entry 

0318  Impact in Pacific 51.4S 128.2W 

Sunday, July 26, 2015

STS-114 (Discovery)

 2005-026A


Discovery will fly LF1/RTF (formerly ULF 1), with ET-121. RSRM-92 is oldest RSRM hardware to fly.

Launch mass 121483 kg; landing mass 121057 kg. Cargo bay mass 13483 kg up, 11395 kg down (not including OBSS). Transfers 1676 kg MPLM, 2994 kg down. Consumables 881 kg.

On ISS, EMUS 3005, 3011 and 3013 with safers 1003, 1004 and 1006. 4 EMU aboard ; 3009 and 3010 will be left on ISS with 3013 and 2 currently on ISS, 3005 and 3011, brought down. SAFERs 1004, 1005 and 1007 to be left on ISS, 1003 and 1006 returned. EVAs will be done in EMUs 3004 and 3017 from Discovery's AL. EV1 is Noguchi, EV2 is Robinson.

EVA 1: Tile DTO 848., ESPAD from LMC to Quest; power cables for ESP-2; replace GPS antenna 2 on S0; OBSS scan of DTO box; repair CMG-2 power module; secondary power cable ESP-2 to S0, behind CETA carts.

EVA 2: CMG 1 remove, replace.

EVA 3: P1 VSSA external camera install, SSRMS install ESP-2, install MISSE PEC 5 (from AL) on P6, retrieve MISSE PEC 1/2 from Quest, retrieve FGRF from ESP2 to stbd TSA. end EVA, SSRMS grapple MLPM.

VSSA on ESP-2, cameras in AL; VSSA to AL to assemble with cameras, then P1.

After MECO, an enhanced ET photo survey will be conducted. The RMS with extension boom will be used to survey the exterior of the Shuttle; this will take one flight day. On approach to Station, at a distance of 180m Atlantis will stop and make a 360 degree turn in pitch to allow imaging from the Station.

An EVA will be conducted to carry out tile repair experiments inside the payload bay.

One of the control moment gyros in Z1 will be replaced. MISSE 1 and 2 will be retrieved, and replaced with PEC-5.

NASA has released its preliminary Return To Flight plan. I give some of the hardware highlights below.

Procedures are being developed for TPS inspection from ISS on approach. If repair were needed, Atlantis would first dock, then grapple ISS with the RMS, then undock while still attached by the RMS, rotating to place the appropriate part of the Orbiter in easy access to spacewalkers using the Station robot arm.

In September, inspection and testing on Atlantis' RCC panels and nosecap will be completed and they will be reinstalled on the orbiter.

In November 2003, the External Tank for STS-114 will be delivered with modifications to the bipod attach ramp and several other areas where foam could be lost.

Around November, pads 39A and 39B will be refurbished with recoating of any exposed zinc primer (which was washing off the pad tower and damaging RCC panels).

In December, NASA will install on the new ET a camera which will transmit in-flight photos of the bipod and of the underside of Atlantis. A camera will also be mounted on the nose cone of each SRB. (For STS-115, cameras will also be installed further down on each SRB for a better view of the Orbiter).

In December, ground tracking cameras will be refurbished, with new cameras due for delivery in March.

In January, redesign ET/SRB separation bolt catchers will be installed.

In early 2004, a boom with laser sensor packages will be fabricated for attachment to the RMS arm; it could be used for Atlantis to inspect itself while in orbit.

A tile repair kit will be delivered in early 2004. It's still not clear when an RCC repair method will be ready.

Modifications to the cameras in the Orbiter umbilical well will not be ready for STS-114, and the astronauts will use handheld cameras to image the ET, downlinking the images to Earth.

Atlantis is currently manifested for launch on 2004 March 11, although this is only a planning date - don't book your tickets yet! 


STS-114 
 

DateTimeEventOrbit  

2005 Mar 29   Tow from OPF3 to VAB  
2005 Mar 31   ET mate 
2005 Apr 7   Roll to pad 39B 
2005 May 26   Rollback to VAB 
2005 Jun 4?  Demate from ET/SRB 
2005 Jun   Restack 
2005 Jun 15   Rollout to pad 39B 
2005 Jul 26  1439:00  Launch by Shuttle  LC39B 
 1441:01  SRB sep 
 1441  Small debris drop from ET 
 1441:12  OMS Assist 2:15 
 1443:29  OMS ASS CO 
 1447:25  MECO  
 1447:47  ET sep  58 x 220 x 51.6 (PAO) 
   54 x 229 x 51.6 (OMS dV) 
 1517:00  T+38:08 OMS-2 30.4m/s 1:07 
 1518:05  OMS 2 CO  155 x 230 x 51.7  
 1550?  ET reentry at 75 km over 160W 37S 
 1614:45  PLBD open 
 1942:24  OMS 3 NC-1  226 x 285 x 51.7  
 1943:44  OMS 3 CO 
2005 Jul 27  0800?  Unberth OBSS 
 0655:31 OMS-4 NC-2  90.10 270 x 287 x 51.6 
 0656:01  OMS 4 CO 
 0724  RMS grapple OBSS 
 1315  Complete OBSS nose inspection 
 1544  Restow OBSS 
 1704s NC3  
2005 Jul 28  
 0628:34  OMS-5 NH 62fps 40s 
 0629:14  OMS-5 CO 
 0715:35  OMS-6 NC4 65fps  
 0716:16  OMS 6 CO 
 0742:22s  NCC 
 0840:04  OMS 7L TI burn 8fps 
 0840:15  OMS 7 CO 
 0900s  MC1 
 0930s  MC2 
 0947s MC3 
 0957  MC4 burn 
 1010s  +R-bar (nadir) stop 200m 
  Imaging 
 1039s forward to V-bar, 100m 
  Approach along V-bar 
 1118 Dock  
 1250  Hatch open 
 1354s SSRMS grapple, unberth OBSS 
 1544s  SSRMS handoff OBSS to RMS  
  OBSS/RMS out of way 
2005 Jul 29 
  SSRMS-B? grapple lab 
  SSRMS-A? ungrapple MBS PDGF-1 
 0544s SSRMS grapple MPLM 
 0644s  MPLM unberth 
 0709s  Begin connecting MPLM to Unity 
  Dock MLPM to ISS 
 0924s  SSRMS ungrapple MPLM  
 0940? SSRMS A? grapple MBS PDGF-1 
  SSRMS B? ungrapple Destiny  
  OBSS survey 
 1500? MPLM HO to ISS 
 1630? FD4 close ISS hatch to OV 
 1700? Depress OV to 10.2psi 
  Depress Quest CL  
2005 Jul 30   FD5 EVA-1 
  SSRMS B? grapple Destiny 
  SSRMS A? ungrapple MBS 
 0935? Depress ODS airlock 
 0943  HO  
 0946 Batt power 
 1000? Egress from ODS 
 1005? Translate to Quest CL hatch  
 1010  In vicinity of CL hatch 
 1012  CL TC open  
 1013  Open Quest CL hatch (Soichi) 
 1013  Noguchi ingress CL 
 1017  egress CL 
 1020? Close ODS hatch  
 1022  Robinson working at ODS hatch 
 1024  ODS TC closed 
  Repress ODS  
  Lawrence, etc. transfer to ISS from OV to control SSRMS 
 1036  Robinson opens DTO box on LMC 
  Working on tile experiments 
 1109  Reopen ISS hatches 
 1235  Noguchi get ESP power cables from ODS TSA 
  Robinson working on ESPAD on ICC 
 1250  Noguchi inspects trunnion pin cover 
  Noguchi to cable worksite on Quest 
 1259  Unberth ESPAD: Robinson on SSRMS  
 1302  SSRMS moving Robinson/ESPAD out of bay 
 1315  Working near ESPAD install location 
 1320  Problems getting soft dock of ESPAD to Quest 
 1325  ESPAD soft docked to Quest 
 1328  Noguchi in CL to get GPS antenna 
 1337  Noguchi egress CL 
 1338  CL TC closed 
 1344  Berth ESPAD to ISS Quest complete 
 1407  Replacing GPS antenna No. 2 on S0, Noguchi 
 1410  CMG-2 electronics patch by Robinson 
 1420  GPSA soft docked to S0 
 1444  GPS antenna work complete 
 1450? Robinson remove MISSE 1 from Quest 
 1500  Rerouting cables in S1 for ESP 
 1504  Begin cleanup and LMC photography 
 1526  Retrieve MISSE 2 from Quest 
 1540  In PLB 
  Close ISS hatch 
 1553  Start to depress ODS from outside 
 1557  3.5 psi 
 1602  Depress ODS complete? 
 1603  HO  
 1604  Ingress ODS Robinson 
 1619? Ingress ODS Noguchi 
 1621  TC closed 
 1627  HC  
 1636  Repress 
2005 Aug 1   EVA-2  
 0829  Depressing airlock 
 0832  5psi, pause 
 0834  Resume depress 
 0835  3psi 
 0837  1psi 
 0838  Depress to 0.7psi 
 0841  HO  
 0842  Batt power 
 0850  Noguchi egress 
 0853  Noguchi at PMA 
 0901?  Robinson egress 
 0904  ODS HC  
 0908? ODS repress 
 0925  EV1/EV2 at Z1 truss 
 1000  Unbolting CMG-1 
 1013  CMG-1 free within housing 
 1015  Unberth CMG-1 from Z1 by Noguchi on SSRMS 
 1045  Installing CMG-1 on ball stack on LMC 
 1056? CMG-1 stashed on LMC  
 1113  CMG-1R unberth 
 1118  New CMG-1R stashed on LMC  
 1134  CMG-1 berthed on LMC 
 1210?  CMG-1 work finished 
 1215? Begin to retrieve CMG-1R from ball stack 
 1220  Noguchi and CMG-1R moving away from PLB on SSRMS 
 1236  Noguchi near Z1 
 1248  CMG-1R soft dock to Z1 
 1259  CMG-1R bolted 
 1307  Connect power cable to CMG-1R 
 1312 Cable connections complete 
 1337  Noguchi on arm, heading back to CMG 
 1344  Reseat power connector 
 1408  Retrieving tools from ETSD on PMA 
 1425  On truss at CETA 2, tools for RJMC 
 1445  Try to open tool box in PLB  
  for TGF prybar and forceps 
 1513  Open tool box after some trouble  
 1523  TC open  
 1523  Begin ODS AL depress 
 1527  3.5 psi  
 1529  ODS AL depress complete (0.7 psi) 
 1531  HO  
 1532? Ingress Robinson 
 1538? Ingress Noguchi 
 1541  TC closed 
 1544:50? HC  
 1556  Repress 
2005 Aug 2  
 1139s  SSRMS grapple ESP-2  
  SSRMS unberth ESP-2 
2005 Aug 3   EVA-3 
 0834  Prebreathe complete 
 0839  5.0 psi  
 0842  Resume depress 
 0844  2.2 psi 
 0845  1.0 psi  
 0846  Depress complete 
 0847  HO  
 0848  Battery power 
 0855  Noguchi egress 
 0902  Robinson egress 
 0903  ODS HC  
 0905  Repress ODS  
 0914  At ESP-2 near Quest 
 0939  Ready-to-latch soft mate 
 0942  ESP-2 installation latched  
 0954  Bolted partially 
 0955  Problem with alignment 
 1015  ESP-2 relatched to fix alignment 
  ESP-2 bolted 
 1027  ESP-2 ungrapple 
 1048  Remove FGRF from ESP-2 
 1108  Installed MISSE 5/PCSAT-2, opened 
 1112 Install complete 
 1122 Noguchi imaging from P6 top 
 1125 Noguchi climbing down 
 1126  Robinson stowed ESP-2 FGRF 
 1129 SSRMS A? ready to grapple MBS 
 1131 SSRMS B? ungrapple Lab 
  Tile gap repair  
 1215  Robinson waiting underneath Shuttle 
 1246  First gap filler removed by Robinson 
 1254  Second gap filler removed 
 1330  In PLB cleanup  
 1334  Robinson egress arm  
  Retrieve APFR 
 1405  Noguchi install extender tool on ESP-2 
 1407  ODS TC open, Robinson  
 1412  Depress ODS AL, at 2psi 
 1413  At 1psi 
 1414  ODS HO 
 1416  Quest HC 
 1418  Quest TC closed 
 1418  Quest AL repress 
 1425  Begin OBSS blanket imaging 
 1428  Ingress Robinson 
 1432  Ingress Noguchi 
 1433  TC closed 
 1439  Hatch closed 
 1449  Repress 
 
2005 Aug 5 
  SSRMS grapple Raffaello 
 1142  SSRMS unberth Raffaello 
 1301  SSRMS lowering R into PLB 
 1303  MPLM berthed and latched 
 1312  SSRMS ungrapple MPLM 
 1355  SSRMS grappple OBSS 
 1358? RMS ungrapple OBSS  
  Stow OBSS via SSRMS  
  Stow RMS  
2005 Aug 6  
 0514  Hatches closed to ISS 
 0723:45  Undock 
 0751 Along +Vbar to 120m 
 0751  Begin flyaround 
 0801  To +Rbar 
 0812  To -Vbar 
 0823  To -Rbar 136m 
 0837  to +Vbar 
 0837  Sep-1 
 0849 To +Rbar 580m 
 0905  Sep-2 
2005 Aug 7   Mass 107671 kg  346 x 358 x 51.6 
2005 Aug 8    
 0510 Close PLBD 
 0921 Open PLBD (weather waveoff) 
 1219:00  OMS-8 OA 24s 12.4m/s 
 1219:25  OMS-8 CO 
2005 Aug 9  0522:33 Close PLBD  
 1106:18  OMS DO 2:42 83.5 m/s over 12 19S 53 19E 
 1109:02  OMS DO CO  40 x 353 km (MR) 
 1140:02  EI 
 1211:23  Landing RW22 EAFB  
 1212:36  Wheels stop 
2005 Aug 19  1532  NASA 905 takeoff from DFRC 
 1845  NASA 905 land at Altus AFB, OK 
 2115  NASA 905 TO from Altus 
 2235? NASA 905 land at Barksdale 
2005 Aug 21  1125  NASA 905 TO from Barksdale 
 1358 NASA 905 land at KSC RW15 

November 20,2006

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