Soyuz TMA-22 (Astraea)

 2011-067A

---

Crew were Anton N. Shkaplerov (KDR), Anatoliy A. Ivanishin, BI-1, and Dan Burbank, BI-2. 

Spacecraft 11F732A17 No. 232, mission 28S. Mass 7220 kg (1259 BO, 2918 SA, 880 prop, so PAO 3043 kg full 2163 dry. Undocking mass 6891 kg.

TMA22
Date	Time	Event	Orbit
2011 Nov 14	0414:04	Launch by Soyuz-FG No. 38	KB LC1-5
	0422:52	Sep from Blok-I
	0803:47 DV1 69s 28m/s
	0841:08 DV2 58s 24m/s
2011 Nov 15	0503:18	DV3 6.1s 2.0m/s 7.6 kg
2011 Nov 16
	0501	DV5 850m
	0507	In flyaround
	0514	Range 200m
	0516	Complete flyaround, 180m
	0517	Begin final approach
	0524:08	Docked with Poisk
	0836	Hatch open
2012 Apr 27
		Crew to Soyuz
	0512	HC (ISS report)
	0604	HC?
	0818:19	Undock
	0821	Sep burn
	1049:26	DO 4:14 115.2m/s
	1117:53	SA/BO sep, 140 km
	1121:13	Entry
	1130	Para deploy
	1144:57s	Landing 51 01N 67 10 E

The Best Laid Plans

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Cygnus CRS-3 (Deke Slayton)

 2014-F02

---

Cygnus ORB-3 mission. 5854 kg launch mass. 2290 kg upmass, 1714 kg down for disposal. If PCM is 1677 kg dry, then service module is 1887 kg. Antares engines E15,E16 and Castor 30XL, first flight of enhanced Antares 130. One of the AJ-26 engine turbobumps failed just after launch, and the vehicle fell back towards the pad. Range safety destruct completed a powerful explosion, destroying rocket and cargo and marking the end for the AJ-26-engined Antares design.

ORB-3 actual
Date	Time	Event	Orbit
2014 Oct 28	2222:30	Launch by Antares 130	MARS Pad 0A
	2222:46	Turbopump failure
	2222:50	Destroyed by RSO
	2222:53	Impact pad area

ORB-3 planned
Date	Time	Event	Orbit
2014 Oct 27	s	Launch by Antares 130	MARS Pad 0A
		T+3:54 MECO, 100 km
		T+4:00 St 1 sep
		T+4:29 Fairing sep
		T+4:34 Interstage sep
		T+4:41 St 2 burn (Castor XL), 140 km, 166s
		T+7:27 St 2 burnout
		T+9:27 St 2 sep, 214 km
2014 Nov 2		Arrival at ISS

Rumour Has It

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Shizuku

 2012-025A

---

'Shizuku' (dewdrop)

JAXA Global Change Observation Mission - Water.

Will observe precipitation, vapor amounts, wind velocity above the ocean, sea water temperatures, water levels on land areas and snow depths.

NEC Toshiba Space? (NECTF??) Mass 1900 kg. Box + 2 panels + dish. 2m box, 2m atetnna, 5m high? 20m? span. Size 5.1 x 17.5 x 3.4m, 1991 kg launch, with 151 kg prop.

H-2A F21 carries a 4/4D-LC fairing with the Arirang 3 satellite in the upper position and GCOM in the lower position. SDS-4 and Horyu 2 are mounted on the lower adapter.

GCOM-1 was at Tsukuba during the earthquake but was not damaged. 700 km SSO

Followon is GCOM-C (Climate)

Launch with Arirang-3, SDS-4 and Houryu-2. The Stage 2 performs post-separation engineering experiments to study upgrades for the propellant system.

GCOM-W1
Date	Time	Event	Orbit
2012 May 17	1639	Launch by H-2A 202	TNSC Y LP1
		T+2:05 SRB-A sep 59 km
		T+4:16 Upper fairing sep (2 halves) 148 km
		T+6:36 MECO 301 km
		T+6:44 St 1 sep 313 km
	1645	T+6:50 SEIG
	1654	T+15:26 SECO-1 676 km
	1655	T+16:16 Kompsat-3 sep
	1658	T+19:21 Adapter sep
	1658	T+19:26 Lower fairing 2 side panels sep.
	1702	T+23:11 GCOM-W1 sep
	1712	T+33:20 SDS-4 sep
	1729	T+50:00 Horyu-2 sep over S Atlantic, 692 km
		Stage 2 thermal experiments

Payload:

• AMSR-2 Advanced Microwave Scanning Radiometer 2 7-89 GHz, 2.7m dia

• Microwave scatterometer

USA-257

 2014-055A

---

This was a LM A2100 satellite on an Atlas V,with an imaging mission for the US government.

CLIO
Date	Time	Event	Orbit
2014 Sep 17	0010	Launch by Atlas V 401	CC SLC41
		T+4:02 BECO
		T+4:08 St 1 sep
		T+4:18 Centaur MES1
		T+4:25 PLF
	0027	T+17:58 MECO-1	176 x 28871 x 27.91
	0257	T+2:47:53 MES-2
	0259	T+2:49:03 MECO-2	11000? x 36000? x 20?
			782.4 8461 x 35038 x 20.7 (UN)
	0301	T+2:51:52 Centaur sep

STS-124 (Discovery)

 2008-027A

---

Launch mass 122072 kg; landing mass 92224 kg. Cargo up 17451 kg; cargo down 3120 kg with OBSS. Non-cargo mass 104621 kg launch, 98070 kg MECO, 89104 kg land.

ET sep mass, 115521 kg. OMS-2 post mass, 112698.3 NC2 mass 112914 kg. Mass at NC3 was 112659 kg, NC4 112529 kg, TI 112412 kg. Cargo to ISS - 15582 kg total, 811 inside, so 14771 outside. Down: 243 kg OBSS, 820 kg inside; Up water/gas: 320 kg.

On ascent, the Left OMS secondary TVC power supply apparently failed; on orbit OMS burns were R OMS only except for deorbit.

An object was seen floating away from Discovery after the control system pre-deorbit checkout on Jun 13. It was identified as a thermal clip from the rudder area.

STS-124
Date	Time	Event	Orbit
2007 Nov 7		OPF3
2008 Apr 26	1117	Tow to VAB-3
2008 May 31	2102:12	Launch
	2104:14	T+2:03? SRB sep
	2104:24	OMS ASS
	2106:47	OMS ASS CO
	2110:39	T+8:24? MECO
	2110:00	T+8:50? ET sep	59? x 228?
			56 x 232 x 51.6 (OMS dV)
			57.5 x 224.0 x 51.95 (TrajData)
	2139:32	OMS-2 2:44
	2142:15	OMS-2 MECO	89.97 231 x 314 x 51.6
	2236:20	PLBD open
	2358:40	OMS-3
	2359:35	OMS-3 CO
2008 Jun 1
	1425:12	NC2 5.9m/s OMS-R 23s
	1425:36	OMS-4 CO
	2328	NC3 RCS 19s
	2120		91.09 322 x 333 x 51.6
2008 Jun 2	1304		91.13 324 x 335 x 51.6
	1344:25	NC4 11s 2.5m/s OMS-5 R
	1344:36	OMS 5 CO
	1417s	NCC
	1516:26	TI 9s 2.6m/s OMS-6 R
	1516:36	OMS 6 CO
	1535s	MC1
	1614	MC2
	1632	MC3
	1639s	MC4
	1656	Range 198m at nadir
	1700	Begin RPM
	1712	Begin flyaround to vbar
	1728	On +Vbar
	1734	71m on approach
	1751	21m
	1802	3m
	1803:22	Docking at PMA2
	1920	PMA2 HO
	1936	Discovery HO
		Exchange seat liners, Riesman to STS crew
2008 Jun 3	1252	SSRMS grapple OBSS on ISS
		EVA-1
	1606	At 5 psi
	1609	2 psi
	1611	1.75
	1616	1.0 psi
	1617	0.8 psi
	1619?	0.7 psi
	1621	HO
	1622	BP
	1629	Fossum egress
	1640	Garan egress
	1717	Unberth OBSS from ISS (KAU attached)
	1731	Begin disconnect of KAU
	1738	OBSS free of truss
	1801	SRMS grapple OBSS
	1812?	SSRMS ungrapple OBSS
	1825	Working on Kibo PM
	1850	SSRMS grapple Harmony
		Kibo launch cover removed
	2010?	SSRMS ungrapple MBS, based on Harmony
	2020	Fossum cleaning SARJ
	2030	SSRMS grapple JEM
	2040	TBA-5 (trundle bearing assy) installed in SARJ
	2049	JEM unberthed
	2100	Testing methods of SARJ cleaning
	2213	JEM close to berthing on Harmony
	2240	JEM berthed RTL on Harmony CBM
	2243	Garan ingress
	2254	Fossum ingress
	2255	TC
	2301	HC
	2301	JEM stage 2 capture, attached
	2306	Repress to 0.1 psi
	2307	Hold repress
	2310	Repress resume (6:48 NASA)
2008 Jun 4	2105	Kibo PM ingress
2008 Jun 5		EVA-2 Fossum, Garan
	1454	1.4 psi
	1500	Depress "just about at vac"
	1503	0.5 psi
	1503	HO
	1504	BP
	1509	Egress Fossum
	1522	Egress Garan
	1550	Translate to end of Kibo, install cameras
	1712	Remove Kibo blankets
	1830	Kibo prep work complete
	1846	Garan to Quest NTA
	1920	Prep old NTA tank for removal
	1945	Fossum to ESP-3
	2032	Remove ETVCG camera from truss CP9
	2102	Port SARJ inspection
	2110	SSRMS ungrapple Kibo
	2150	Ingress Garan
	2201	Ingress Fossum
	2201	TC closed
	2205	SSRMS grapple MT
	2210	HC
	2215	Repress (NASA 7:11)
2008 Jun 6	1817	SSRMS grapple JLM
	1839	Unbolting JLM
	1917	Unberth JLM
	1951	Ready to berth on Kibo PM
	1959	Bolting JLM
	2004	JLM bolting complete
	2013	SSRMS ungrapple JLM
2008 Jun 7	1645?	JRMS initial deploy
2008 Jun 8		EVA-3
	1340	4psi
	1346	1.5 psi
	1348?	Depress?
	1353	HO
	1355	BP
	1400	Egress Garan
	1415	Egress Fossum
	1435	On S1 truss, Garan entering SSRMS
	1455	Unbolting old N2 tank
	1504	old N2 tank released by Garan, 240 kg
	1505	new N2 tank released? from ESP3 by Fossum
	1508	Remove old N2 from S truss, Garan on SSRMS
	1512	SSRMS moving Garan to ESP3
	1518	New N2 stowed on ESP3 handrail
	1530	Old N2 being stowed on ESP3
	1545	SSRSM moving Garan to S1 with new NTA
	1555	Garan arrives S1
	1608	New NTA installed
	1630	Fossum gets dust sample from port SARJ
	1800	Fossum prepping JEM-RMS cameras
	1830	Garan installing new P1 camera
	2012	Fossum ingress
	2015	Ingress Garan
	2023	HC
	2028	Repress
2008 Jun 10	2042	HC to ISS
2008 Jun 11	1141:55	Undock
	1211	Begin flyaround
	1228	Behind ISS
	1237	Below ISS (+rbar)
	1252	Sep-1 burn MET 1548:44, on Vbar
	1320	Sep-2 burn on -Rbar (zenith)
2008 Jun 13	1230?	Rudder thermal clip separates
2008 Jun 14	1132:14	PLBD closed
	1410:12	13/17:08:00.0 OMS Both 2:34 88 m/s (DOL pad)
	1412:47	OMS Deorbit cutoff
	1443:40	Entry interface 120 km
	1515:18	MGTD KSC RW15
	1515:30	NGTD
	1516:19	WS

Inmarsat 301

 1996-020A

---

The Inmarsat III series carried L-band maritime communications payloads built by Matra Marconi Space UK. Mass of the satellite was 2068 kg launch, 1100 kg BOL, 860 kg dry. It replaced Inmarsat II F-1 as the IOR satellite at 64E.

Inmarsat III G1
Date	Time	Event	Orbit
1996 Apr 3	2301:01	Launch by Atlas IIA (AC-122)	CC LC36A
	2303	BECO
	2303	Booster sep
	2304	Fairing sep
	2305	SECO
	2305	Atlas sep
	2306	Centaur MES1
	2311	Centaur MECO-1
	2323?	Centaur MES2
	2325?	Centaur MECO2
		Centaur sep
1996 Apr 3			642.95 1019 x 35577 x 21.9
1996 Apr 5			642.95 1020 x 35575 x 21.8
1996 Apr 6	1024?	AKM burn
1996 Apr 8			1414.5 35174 x 35549 x 2.7
1996 Apr 14			1436.01 35758 x 35811 x 2.7 GEO 27.6E
1996 Apr 25			1435.96 35761 x 35806 x 2.6 GEO 27.8E
1996 Apr 29		mv out
1996 May 3			1424.52 35546 x 35573 x 2.6 GEO 51.0E+3E
1996 May 12			1436.11 35780 x 35793 x 2.6 GEO 63.9E
1996 Sep 25			1436.04 35767 x 35803 x 2.4 GEO 64.1E
1999 Oct 17			1436.09 35769 x 35803 x 0.1 GEO 63.9E
2006 Aug 3			1436.06 35766 x 35805 x 0.0 GEO 63.7E
2010 Dec 26			1436.10 35764 x 35809 x 0.1 GEO 64.5E
2013 Jul 30			1436.09 35763 x 35809 x 1.2 GEO 64.4E

Iridium 51

1998-018A

---

Iridium 51 was launched on a CZ-2/SD.

Iridium 51
Date	Time	Event	Orbit
1998 Mar 25	1701	Launch by CZ-2SD
	1703?	Stage 1 sep
	1704?	Fairing sep
	1707?	Stage 2 MECO
	1710?	Stage 2 VECO, sep
	1749?	SD burn
	1751	Sep from SD	675 x 680 x 86.4
1998 Mar 25	1756?	SD orbit lower	92.75 195 x 623 x 86.3
1998 Apr 1			98.31 675 x 680 x 86.4
1998 Apr 3			100.15 762 x 768 x 86.44
1998 Apr 5			100.39 774 x 779 x 86.4
1998 Apr 10			100.40 775 x 779 x 86.4
1998 May 16		Begin orbit lower	100.40 774 x 780 x 86.4
1998 May 18			99.99 754 x 759 x 86.4
1998 May 21		Reach storage orbit	99.81 747 x 751 x 86.4
2004 Jun 29			99.78 746 x 750 x 86.5
2012 Jun 27			99.80 747 x 750 x 86.5
2012 Jul 17		In constellation	100.40 776 x 779 x 86.4
2013 Jan 30			100.40 776 x 779 x 86.4

ISEE 3

 1978-079A

---

The third satellite in the ISEE program, NASA-GSFC's ISEE C or ISEE Heliocentric satellite, was designed to study the solar wind from a unique orbit around the L1 Lagrange point of the Earth-Sun system. It was launched on 1978 Aug 12 at 1512:16 by a Delta 2914 from Cape Canaveral into Earth orbit. The Delta second stage entered a 100.9 min, 176 x 1436 km x 28.7 deg orbit. The Star 37E third stage separated and ignited to insert ISEE 3 (International Sun-Earth Explorer 3) into a 180 x 1151164 km x 28.9 transfer orbit. The DV1 course correction burn was made on Aug 13. ISEE 3 passed lunar orbit on Aug 15, and DV2 and DV3 correction burns were made on Sep 6 and Oct 16. On Nov 20, ISEE 3 entered a `halo orbit' of radius 100000 km and period 6 months around the Earth-Sun L1 point, 235 Earth radii toward the Sun along the Earth-Sun line. This libration point orbit was unstable but required only a small amount of fuel to keep the spacecraft on track. The first halo orbit was complete on 1979 May 14.

The second phase of ISEE 3's mission began on 1982 Jun 10, when a small burn made it leave the vicinity of L1 and head towards the Earth's magnetotail. It passed the magnetotail on Oct 14-24, at an Earth distance of 400000 km. It reached apogee at 1200000 km on Nov 23. It passed the magnetotail again on Dec 22 with a perigee of 70000 km. During 1983 Jan it entered the magnetotail on the way to apogee (1400000 km on Feb 8) at which point it made a course correction maneuver. It left the magnetotail on Mar 30 and the same day made its first lunar flyby at a distance of 20000 km. It passed through the magnetosphere on Apr 3-19, flew past the Moon again into the magnetotail (Apr 26-Sep 4) with an apogee at L2 on Jun 30. Two more lunar flybys were made on Sep 28 and Oct 22, followed by trim burns on Nov 10 and Nov 23, the first targeting at lunar impact and the second refining the trajectory to miss the lunar surface by 120 km. ISEE 3 skimmed the surface at 120 km on its 5th flyby at 1840 UT on 1983 Dec 22, the resulting gravity assist sending out into solar orbit to begin the third phase of its mission.

ISEE 3 was now renamed the International Cometary Explorer (ICE). The ICE probe left the Earth Moon system and coasted in solar orbit until a final course correction in Mar 1985 left it on target to pass through the tail of comet P/Giacobini-Zinner. It passed within 3000 km of the cometary nucleus on 1985 Sep 11, as the comet descended through the ecliptic plane. On Oct 31 it passed 140 million km upstream of comet P/Halley, and on 1986 Mar 28 it passed 305 million km upstream of Halley, studying the solar wind in the vicinity each time. Sometime in 1986 a small maneuver changed the orbit to a 355 day period. It is hoped that on 2014 Aug 10 the ICE probe will be captured by lunar gravity as it passes the Earth-Moon system. ICE was shut down in May 1997, but the carrier signal was tracked again in 2008.

ISEE 3/ICE
Date	Time	Event	Orbit
1978 Aug 12	1512:16	Launch by Delta
		T+0:38 SRM 1-6 out
		T+0:39 SRM 7-9 on
		T+1:18 SRM 7-9 out
		T+1:27 SRM 1-9 sep
		T+3:45 MECO
	1514	T+3:54 Thor sep
	1514	T+3:56 SES-1
	1516	T+4:56 Fairing
	1521:00	T+8:44 SECO-1	157 x 285 x 28.5
		47 min coast
	1605:47	T+53:31 SES-2 25s
	1606:08	T+53:52 SECO-2	176 x 1436 x 28.7
	1607:08	T+54:52 St 2 sep
	1607:49	T+55:33 TES 40s
	1608:33	T+56:17 TECO	180 x 1151164 x 28.9
	1609:46	T+57:30 Stage 3 sep, retro
	1610	Injection
	1624	Yo-yo despin
	1640	Deploy booms
1978 Aug 13	0621	Pass EL1:4
	1010	DV1 17.9m/s
	1110	End DV1
1978 Aug 15		Lunar distance
	1316	Begin XY antenna deploy
	1452	Complete XY antenna deploy
1978 Aug 31		Range 1.2Mkm
1978 Sep 6	1804	DV2 24.8m/s
	1945	End DV2
1978 Nov 20	1834	HOI DV3 14.0m/s
	2039	End DV3
1978 Nov 20		L1 Halo Orbit 100000 km rad
1978 Dec 6	1916	Z-axis antenna deploy part 1
1979 Jan 9	1900	Z-axis antenna deploy part 2
1979 May 14		Completed first halo loop
1982 Jun 10		TCM 4.5m/s
1982 Jun 10		Magnetotail Transfer Orbit
1982 Aug 10		TCM 0.5m/s
1982 Oct 14		Begin pass through geotail
1982 Nov 23		Apogee 1: 1200000
1982 Dec 15		TCM 0.1m/s
1982 Dec 22		Perigee 2: 70000
1983 Feb 8		Apogee 2: 1400000 at L2,
1983 Feb 8		TCM 34.1m/s
1983 Mar 1		TCM 1.1m/s
1983 Mar 22		TCM 0.35m/s
1983 Mar 30	1747	Lunar flyby S1: 21307 km
1983 Apr 2		TCM 0.1m/s
1983 Apr 3		Perigee 3: 50000
1983 Apr 13		Apogee 4: 500000
1983 Apr 19		Perigee 4: 50000
1983 Apr 23	0103	Lunar flyby S2: 22875 km
1983 Jun 1		TCM 27.0m/s
1983 Jun 30		Apogee 5:  1500000 near L2
1983 Jul 1		TCM 2.2m/s
1983 Aug 12		TCM 0.31m/s
1983 Sep 20		TCM 0.03m/s
1983 Sep 27	1800	Lunar flyby S3: 24527 km
1983 Oct 1		TCM 0.16m/s
1983 Oct 2		Perigee 5: 70000
1983 Oct 10?		Apogee 6: 500000?
1983 Oct 12		TCM 0.15m/s
1983 Oct 15?		Perigee 6: 70000?
1983 Oct 21	1632	Lunar flyby S4, 19178 km
1983 Oct 25		Exit geotail: 400000
1983 Nov 10		TCM 6.5m/s, target S5
1983 Nov 23		Trim burn at apogee 0.16m/s
1983 Nov 23		Apogee 7: 1250000
1983 Dec 22	1845:15TT	Lunar flyby S5, 119.4 km
1983 Dec 27		Leave Earth-Moon system, 400000
1984 Jan 2		Leave EM sphere, L1	355d 0.93 x 1.03 AU x 0.1
1985 Jun 5		dV 39m/s targeting to 17800 km (from 62000 km)
1985 Jul 9		dV 1.2m/s to 9880 km targeting
1985 Sep 8	1200	dV 2.3m/s begins 4:19
	1619	End burn
1985 Sep 11	1059:40	Enter GZ magnetotail
1985 Sep 11	1102:22	G-Zinner 7870 km at 21km/s rel
	1107:40	Leave GZ magnetotail
1985 Oct 31		Halley 140Mkm
1986 Feb 27		1.2m/s dV, 2014 targeting 1.51m/s
1986 Mar 28		Halley 305 Mkm
1986 Apr 7		38.5m/s dV, 2014 targeting plane change
1986 Apr?		Perilin etargeting 0.4m/s
1990 Jan			0.93 x 1.03 AU x 1.0
1997 May 5		Decommissioned
2008 Sep 18	2049	Carrier signal tracked by DSS-14 for 3h
2014 May 19			354.57d 0.927 x 1.034AU x 0.06
2014 Jul		Reactivated by ISEE3Reboot Team
2014 Jul 8	1747	TCM RE=5.3Mkm
2014 Jul 12			355.09 0.927 x 1.036 x 0.06
2014 Jul 23		Begin interplanetary citizen science mission
2014 Jul 31	0319	In Earth L1 radius
2014 Aug 3	1920	In Earth sphere 929000 km
2014 Aug 9	0308	Perigee	178398 x -492663 x 42.5
2014 Aug 10	1015	In Lunar sphere, 66000 km
2014 Aug 10	1927	Lunar flyby	15938 x -22202 x 33.7
2014 Aug 11	0435	At 66000 km, leave lunar sphere
2014 Aug 14	0739	At 929000 km leave Earth sphere
2014 Aug 17	1904	At 1.5MKm leave Earth L1 radius
2014 Dec 3			421.94d 1.012 x 1.190AU x 1.17 deg

Soyuz TMA-10 (Pulsar)

 2007-008A

---

Flight 14S with Expedition 15. RKKE Fyodor Yurchikin, Pol. Kotov , Charles Simonyi. Kotov was Soyuz commander and ISS BI-1, with Yurchikin as Soyuz BI and later ISS commander.

Soyuz TMA No 220 with Soyuz FG 019. Mass 7220 kg.

Carried the Biorisk-MSN-2 experiment. Biorisk was moved to Pirs, and installed on Zvezda during the 2007 Jun 6 EVA. It contained 3 containers; no. 1 was retrieved on 2008 Jul 15 and landed on 2008 Oct 24 in Soyuz TMA-12.

During landing on Oct 21, the PAO failed to separate at the correct altitude, eventually burning away. Entry was ballistic, resulting in touchdown 340 km W of Arkalyk, SW of the usual site.

TMA10
Date	Time	Event	Orbit
2007 Apr 7	1731:14	Launch by Soyuz-FG
		T+1:53 SAS sep
		T+1:58 Strapons sep
		T+2:37 GO sep
		T+4:47 Blok A sep
		T+4:57 KhO sep
		T+8:45 MECO
		T+8:48 Blok I sep
2007 Apr 9	1853	Begin flyaround, 400m?
	1900	At 200m, skeep
	1910	Docked with Zarya
	2030?	HO
2007 Sep 27	1520s	HC to Zarya
	1920	TMA-10 undock Zarya
		Back off 25-30m
		Translate
	1940	Begin final approach
	1947	TMA-10 dock Zvezda
2007 Oct 21	0400?	HC to ISS
2007 Oct 21	0714	Undocked Zvezda
	0717	Sep burn 15s 0.6m/s
	0947:07	Deorbit 115.2m/s
	0951:28	Deorbit cutoff
	1011:25	Modules sep fail	-46? x 344 x 51.6
	1014:15	Entry interface 102km
	1015?	Modules sep 80 km
	1018	switch to ballistic reentry mode
	1035:49	Landed W of Arkalyk

Progress M-14M

 2012-004A

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Mission 46P, Spacecraft 11F615A60 No. 414. Launch mass 7290 kg, docking mass 6933 kg. Planned mass at 2nd docking 6783 kg. Empty 6439 kg.

Cargo mass 2669 kg including 63 kg of accounted EVA hardware.

After undocking, the Radar-Progress experiment used thruster firings to study the ionosphere.

PM14M
Date	Time	Event	Orbit
2012 Jan 25	2306:40	Launch by Soyuz-U	KB LC1
	2311	Blok-A sep
	2315:29	Blok-I sep	88.79 185 x 243 x 51.6
2012 Jan 26	0307:33	DV1 62.8s 24.9m/s
	0338:35	DV2 27s 10.8m/s	89.76 235 x 289 x 51.6
2012 Jan 27
	0015	DV3 17s 1.2m/s
	1837		89.77 234 x 291 x 51.6
	2346	In flyaround
	2351	Complete flyaround, skeep at 200m
	2358	195m begin final approach
2012 Jan 28	0008:51	Docked to Pirs
	0018	Hard dock
	0352	HO
2012 Feb 6		Fuel transfer to SM
2012 Feb 7		Oxidizer transfer
2012 Feb 8		Fuel transfer to SM
2012 Feb 9		Oxidizer transfer
2012 Apr 2		fuel/oxid. transfer
2012 Apr 19	1103:38	Undocked from Pirs	388 x 408 x 51.6
	1107	Sep burn 15s 3m/s
		Radar-Progress experiment
2012 Apr 23	1037:58	RP1 10s 4.5m/s	92.49 386 x 406 x 51.6
2012 Apr 24	1119:22	RP2 9s 4.5m/s
2012 Apr 25	1023:54	RP3 10s 4.5m/s
2012 Apr 26	0927:52	RP4 10s 4.4m/s
	1104:56	RP5 9s 4.9m/s
2012 Apr 26			92.35 360 x 418 x 51.6
2012 Apr 27			92.34 358 x 420 x 51.6
2012 Apr 28	1347:00	Deorbit 3:11 93.2m/s	355 x 421 x 51.6
	1350	DO CO	54 x 403 x 51.6
	1425?	Entry
	1439	Impact 50S 180W