SERVIS-2

 2010-023A

---

Space Environment Reliability Verification Integrated System. SERVIS-2 will launch on Rokot from Plesetsk in 2010. Mass 740 kg. Orbit 1200 x 1200 x 100.42. Funded by Ministry of Economics, Trade and Industry (METI) and NEDO (New Energy and Industrial Technology Dev. Organization); operated by Institute for USEF, Tokyo. Project is to space-qualify commercial off-the-shelf parts for use on spacecraft.

Size 2.3 x 1.5m x 1.4m, 10.2m span.

SERVIS-2
Date	Time	Event	Orbit
2010 Jun 2	0159:12	Launch by Rokot	PL LC133/3
	0201:17	T+2:06 St 1 sep 68 km	-5911 x 158 x 99
	0201:20	St 2 burn
	0202:03	T+3:09 Fairing 121 km	-5705 x 184 x 99
	0204:19	St 2 MECO
	0204:20	T+5:19 St 2 sep 238 km 8 deg 5.656 km/s	-4058 x 309 x 99
	0204:26	T+5:25 Briz MES-1
		St 2 impact at 77 11 N 75 18W 3868 km range
	0213:18	T+13:47 MECO-1	153 x 1177 x 99.45
	0314:05	T+1:15:04 MES-2
	0314:50	T+1:15:48 MECO-2
	0336:30	T+1:37:30 Briz sep from SERVIS-2	1186 x 1210 x 100.4
	0346:31	T+1:47:30 Briz MES-3 lower orbit
	0349:11	T+1:50:10 Briz MECO-3	877 x 1206 x 100.6

Payload:

• CPTU Commercial Parts Test Unit (SRAM, DRAM, Flash Mem, FPGA)

• COTS COTS equipment

  • LIBA Li Ion (Mn type) Battery System with Automotive Technology

  • ADMS High Assurance Data Management System

  • CRAFT Fault Tolerant Computer with CRAFT system

  • PPRTU Plug and Play Remote Terminal Unit

  • HPDC High Performance Data Compressor

  • APE Advanced Positioning Experimental Module

Galaxy 9

 1996-033A

---

The Hughes Communications Galaxy IX satellite was launched to relieve a shortage of US domestic cable TV distribution capacity. At the time of launch, its transponders were leased by Viacom, TVN, and Global Access. Galaxy 9 was launched by a Delta 7925 rocket from Cape Canaveral. Mass at launch was 1400 kg.

Galaxy 9
Date	Time	Event	Orbit
1996 May 24	0110:00	Launch by Delta 7925	CC LC17B
		Azimuth 97.5 deg
	0114:28?	MECO
	0114	SES-1
	0120?	SECO-1	185 x 190? x 28.8
	0132?	SES-2
	0132?	SECO-2	190 x 1870? x 28.5
	0226?	SES-3
	0226	SECO-3	330? x 1880? x 25.8?
	0226:40	T+1:16:40 St 2 sep
1996 May 24	0227:17	Star 48 burn
	0228:44	TECO
	0231	Star 48 sep
1996 May 24			686.21 1878 x 36906 x 22.9
		SES-3?
		SECO-3?
1996 May 24		Delta depletion	337 x 1574 x 25.83
1996 May 26	0530?	Star 30C burn
1996 May 29			1462.47 35769 x 36832 x 0.1 GEO 96.7W+6.5W
1996 Jun 8			1435.96 35772 x 35795 x 0.0 GEO 123.0W
1996 Jun 20			1436.07 35777 x 35794 x 0.0 GEO 123.1W
1997 May 16		To Panamsat	GEO 123W
1999 Oct 17			1436.06 35781 x 35790 x 0.0 GEO 122.9W
2000 Mar 10		Move to 127W
2000 Apr 18			1436.04 35782 x 35798 x 0.0 GEO 126.9W
2006 Jul 6			1436.11 35780 x 35793 x 0.0 GEO 90.9W
2006 Jul 25		mv out
2006 Aug 4			1434.54 35746 x 35765 x 0.1 GEO 84.4W+0.4E/d
2006 Sep 2		Move in at 74W	1436.09 35781 x 35790 x 0.0 GEO 74.2W
2007 Aug 21			1436.10 35781 x 35791 x 0.0 GEO 74.2W
2007 Aug 22		move out
2007 Aug 30		move in at 81W
2007 Sep 2			1436.39 35770 x 35814 x 0.0 GEO 81.0W
2010 May 1			1436.13 35777 x 35797 x 1.6 GEO 81.0W

The Classic Guide to King Arthur

 https://welib.org/md5/5cc039e3e2f94a6bd3279d0ccf043235

GIOVE-A

 2005-051A

---

The 600 kg GSTB-v2/A testbed satellite for Galileo, under a contract let by ESA to SSTL. GIOVE is Galileo In-Orbit Validation Experiment.

Galileo will be the European global navigation satellite system.

The first satellite will be a 600 kg SSTL GEMINI (MOSAIC) bus launched by Starsem Soyuz to 23616 x 23616 x 56.0. Size is 1.3 x 1.8 x 1.7m with 11m? span.

Soyuz-FG No. Zh15000-015 with Fregat No. 1009.

Control from Chilbolton and RAL.

The MERLIN monitor gives proton flux, heavy ion spectrum, total dose, internal charging and surface charging. It is derived from the earlier CREDO (Cosmic Ray Effects and Dosimetry Experiment) and SURF (electrostatic charging monitor) experiments.

In Sep 2009, the satellite raised its orbit above the nominal constellation, but continued in operation. In 2012 the nav payload was switched off but the satellite continued to collect radiation data.

Giove A
Date	Time	Event	Orbit
2005 Dec 28	0519:08	Launch by Soyuz-FG	KB LC31-6
		T+1:58 Strapons sep
		T+4:13 Fairing sep
		T+4:46 Blok I MES
		T+4:47 Blok A sep
		T+4:57 KhO sep
	0527:56	T+8:48 Blok I sep	58? x 190 x 51.8
	0528:57	T+9:49 Fregat MES-1
	0529:17	T+10:09 Fregat MECO-1	220 x 220 x 51.8?
	0557:33	T+38:25 Fregat MES-2
	0602?	Blok-I reentry over Pacific
	0607:29	T+48:21 Fregat MECO-2	220 x 23600 x 56?
	0855:57	T+3:35:59 Fregat MES-3
	0859:08	T+3:40:00 Fregat MECO-3
	0901:39	T+3:42:00 Fregat sep	23011 x 23258 x 56.1
2007 Oct 19			846.12 23229 x 23281 x 56.0
2009 Sep 16			849.61 23307x 23365 x 56.1
2009 Oct		orbit raise to reserve orbit	849.64 23308 x 23366 x 56.1
2012 Jun 20			894.69 23314 x 23362 x 56.2
2012 Jun 21	1230?	Orbit raise
2012 Jun 30		Nav payload switched off
2012 Jul		SGR-GEO payload activated
2012 Jul 3			894.89 23321 x 23365 x 56.2
2012 Nov		Still operating SGR-GEO

Seventeen: September 2012

 https://welib.org/md5/ad03830035fd52a6df9caed282451e80

Seventeen: May 2011

 https://welib.org/md5/08edba9520f41b7be060f73cf1406eeb

Millennium Falcon: Star Wars Legends

 https://welib.org/md5/723db6c4b2c8ca194dc20da1dbb97191

Asiasat 2

 1995-064A

---

The Asiasat 2 satellite was launched in Nov 1995 by a CZ-2E. This marked the first successful use of the Chinese-built solid EPKM perigee stage to insert a satellite into geostationary transfer orbit. The EPKM stage uses the solid SPTM-17 motor; it was fired on the second southbound equator crossing. The launch was rougher than expected and the antenna feed horns seem to have been knocked out of alignment, reducing the amount of the signal reaching the ground. This caused Hong Kong's Star TV to cancel its lease of three Ku-band transponders.

In 2009 Sep, the satellite was acquired by Amos-Spacecom and renamed Amos 5i. It was relocated to 17E. However, a year later it was discovered that the satellite had less propellant remaining than previously believed, limiting its life. It left the 17E slot in Sep 2011 and was moved to 120E for a while before being retired in mid 2012.

Asiasat 2
Date	Time	Event	Orbit
1995 Nov 28	1130:05	Launch by CZ-2E	XSC
		T+2:05 Booster cutoff
		T+2:07 Boosters sep
		T+2:38 Stage 1 MECO
		T+2:40 St 1 sep
		T+3:20 Fairing sep
		T+7:40 St 2 MECO
	1139	T+9:33? St 2 VECO
	1140?	CZ-2E stage 2 sep	187 x 292 x 28.0
	1324	EPKM burn, 89s
	1325	EPKM burnout
	1326?	EPKM sep	220 x 35039 x 25.6
1995 Nov 28			617.02 220 x 35039 x 25.6
1995 Nov 30	0100	LAM burn 31 min (Leros)	717.95 5326 x 35031 x 13.8
1995 Dec 2?		LAM-2
1995 Dec 4?		LAM-3
1995 Dec 4			1403.89 34375 x 35932 x 0.6
1995 Dec 5			1423.30 34556 x 36514 x 0.4 GEO 94.1E+3.3E
1995 Dec 9		mv in	1437.60 35778 x 35853 x 0.4 GEO 100.5E
1995 Dec 27			1436.16 35777 x 35798 x 0.4 GEO 100.5E
1999 Oct 17			1436.12 35777 x 35797 x 0.0 GEO 100.6E
2006 Aug 4			1436.07 35774 x 35797 x 0.0 GEO 100.6E
2009 Oct 10			1436.12 35779 x 35794 x 0.1 GEO 100.5E
2009 Oct 16		Move out of GEO at 1.0 deg/d
2009 Dec 12			1440.11 35840 x 35889 x 0.0
2010 Jan 9		Begin Amos 5i ops at 17E	1436.10 35777 x 35795 x 0.0 GEO 17.0E
2011 Aug 20			1436.00 35772 x 35797 x 0.9 GEO 17.1E
2011 Sep 3			1435.95 35771 x 35796 x 0.8 GEO 17.5E+0.03E/d
2011 Sep 5		Move out	1433.66 35662 x35815 x 0.8 GEO 18.6E+0.6E/d
2011 Oct 14			1432.71 35707 x 35732 x 0.9 GEO 50.9E+0.8E/d
2012 Jan 1		Braking
2012 Jan 9		Move in	1436.02 35770 x 35799 x 1.1 GEO 120.0E
2012 May 18			1436.33 35765 x 35816 x 1.4 GEO 119.3E

Realizing tomorrow : the path to private spaceflight

 https://welib.org/md5/9f4d1bc9d605182c49fe600e5a906629

Ancient Rocketry: Standing on the Shoulders of Giants

 https://content.blubrry.com/spacerockethistory/SRH-2013-02-26-001.mp3

Astra 1E

 1995-055A

---

Astra 1E was launched by Ariane 42L (V79) from Kourou on 1995 Oct 19. It is the first all-digital TV broadcasting spacecraft in the SES Astra fleet. It will be stationed at 19.2E. Mass of the HS-601 satellite is 3010 kg launch, 1803 kg BOL, 1343 kg dry, with a 3.4 x 2.8 x 4.5 m bus, 7.4 m high and 26.2 m span when deployed. 

In mid 2007 it was planned to replace Astra 1E with Astra 1L and move 1E to 23.5E for direct broadcast television services.

Astra 1E
Date	Time	Event	Orbit
1995 Oct 19	0038	Launch by Ariane 42L (V79)	CSG ELA2
	0041	Stage 2 TIG
	0043	Stage 2 sep
	0043	Stage 3 TIG (T+5:28)
	0056	Stage 3 MECO (T+18:20)
	0059	H-10-3 sep (T+21:08)	638.1 504 x 35845 x 4.2
	0059	H-10-3 avoidance burn	653.9 496 x 36656 x 4.2 (H-10-3)
1995 Oct 19			638.13 503 x 35845 x 4.1
1995 Oct 20	0330?	LAM1
1995 Oct 20			837.71 10282 x 35835 x 1.6
1995 Oct 21	2130?	LAM2
1995 Oct 22			1184.15 25659 x 35737 x 0.3
1995 Oct 23	1200?	LAM3
1995 Oct 23			1389.43 33675 x 36060 x 0.2 GEO 6.5W+12.1E
1995 Oct 25		LAM4?
1995 Nov 2			1436.38 35705 x 35878 x 0.1 GEO 14.8E+0.08W
1995 Nov			GEO 14.7E
1995 Nov		Move to 19E
1995 Dec 9			1436.06 35771 x 35800 x 0.1 GEO 19.0E
1996 May 1			1436.04 35761 x 35809 x 0.1 GEO 19.2E
1999 Oct 16			1436.06 35784 x 35787 x 0.1 GEO 19.2E
2006 Jul 28			1436.17 35764 x 35811 x 0.1 GEO 19.2E
2007 Oct 3			1436.06 35765 x 35806 x 0.0 GEO 19.2E
2007 Oct 5		Move out
2007 Oct 20		Move in at 23E	1436.07 35768 x 35803 x 0.1 GEO 23.5E
2010 Jul 29		Move out	1436.15 35771 x 35804 x 0.2 GEO 23.3E
2010 Sep 12		Move in at 5E	1436.08 35769 x 35802 x 0.3 GEO 4.7E
2012 Dec 23			1436.09 35769 x 35803 x 2.1 GEO 4.6E

STS-122 (Atlantis)

 2008-005A

---

Launch mass 121264 kg. Landing mass 93536 kg.

725 kg of middeck ISS cargo up; a similar amount down.

Dan Tani will be returned from station, replaced by Leo Eyharts. Columbus will be docked to Harmony starboard CBM. The PDGF will be moved from the sidewall carrier to Columbus. Atlantis will resupply the ISS with water. The P1 NTA is replaced; the SOLAR and EUTEF experiments are moved from ICC to the EPF.

STS-122
Date	Time	Event	Orbit
2007 Nov 3		Tow to VAB
2007 Nov		Rollout to LC39A
2007 Dec 6		Scrub ECO, T-6h
2007 Dec 9		Scrub ECO, T-8h
2008 Feb 7	1945:30	Launch	KSC LC39A
	1947:34	SRB sep
	1947:44	OMS assist
	1949:37	OMS Ass CO
	1953:53	MECO command
	1954:00	Zero thrust
	1954:15	ET sep	58 x 230 x 51.6
	2023:10	T+37:40s OMS-2 1:44
	2024:54	OMS-2 CO	220 x 230 x 51.6
	2100?	ET reentry
	2135:59	PLBD open
	2137	PLBD open complete	215 x 233 x 51.6
	2322:47	OMS-3 NC1 burn
	2323:02	OMS-3 CO
2008 Feb 8	1242:44	OMS-4 R NC2
	1242:54	OMS-4 CO
	1255	NPC
	2225	NC3	229 x 254 x 51.6
2008 Feb 9	1216:15	OMS-5
	1217:14	OMS-5 CO
	1306:11	OMS-6 NC4	331 x 339 x 51.6
	1307:00	OMS-6 CO
	1437:28	OMS-7 L TI 112164 kg
	1437:39	OMS-7 CO
	1500	MC1
	1526	MC2
	1546	MC3
	1549	1.6 km range
	1610	180m on -Rbar
	1627	Begin RPM
	1632	RPM complete
	1648	90m on +Vbar, skeep
	1650	Approach
	1657	49m
	1705	21m
	1717:15	Docking
	1840	HO to ISS
	2018	SSRMS grapple OBSS
	2033	OBSS unberth
	2053	SRMS grapple OBSS
	2056	SSRMS ungrapple OBSS
	2220	Eyharts IELK swap
2008 Feb 10	1207	91.24 331 x 339 x 51.6
2008 Feb 11		EVA-1 Love, Walheim
	1346	Begin depress
	1400	4.0psi
	1408	0.9psi?
	1412	0.6psi, Depress
	1413	HO
	1415	Battery power
	1426	Walheim egress
	1438	Love egress
	1602	PDGF removed from PLB
	1659	PDGF installed on COF
		COF arm heater cables attached
		COF CBM covers removed
	1933	SSRMS grapple COF
	1956	SSRMS unberth COF
	2125	Walheim preps for removing NTA on P1
	2125	COF approaching mate
	2129	COF RTL on Node 2
	2133	First stage capture
	2144	Stage 2 capture, COF docked
	2152?	Walheim ingress
	2201?	Love ingress
	2208	HC
	2212	Repress
2008 Feb 12	1255s	SSRMS ungrapple COF
	1420?	Crew ingress Columbus
2008 Feb 13		EVA-2 Walheim, Schlegel
	1421	0.7 psi depress
	1422	0.6 psi
	1425	HO
	1427	Battery power
	1440?	Walheim egress
	1448	Schlegel egress
	1628	New NTA removed from ICC
	1700	New NTA temp stowed on CETA; remove old NTA
	1730	Old NTA removed by Walheim, temp stow on CETA
	1742	New NTA installed in P1
	1825	Old NTA in hand on end of SSRMS, at CETA
	1900	Old NTA in ICC
		Columbus trunnion covers
	2050	Walheim ingress
	2057	Schlegel ingress
	2105	HC	91.24 331 x 339 x 51.6
	2112	Repress
2008 Feb 15		EVA-3 Walheim, Love	91.24 331 x 339 x 51.6
	1306?	Depress
	1307	HO
	1309	Battery power
	1316	Walheim egress
	1328	Love egress
	1400	Install handrails on Columbus
	1455	Love on SSRMS removes Solar from ICC
	1530	SOLAR installed on EPF
	1640	Unbolting failed CMG from ESP-2
	1725	Berthing CMG on ICC-L
	1810?	Unberthing EUTEF from ICC-L
	1850?	EUTEF on COF EPF
	1935	Inspecting airlock handrail divot
	2015?	Ingress Walheim
	2020	Ingress Love
	2021	TC closed
	2025	HC start
	2029	HC and locked
	2033	Repress
2008 Feb 16	1218	Reboost ISS
	1300?	Reboost complete	91.30 332 x 343 x 51.6
2008 Feb 17	1759	HC to ISS
2008 Feb 18
	0924:40	Undocking
	0956	120m on +Vbar; begin flyaround
	1008	Atlantis on +Rbar above ISS, 180m
	1019	On -vbar
	1031	Below ISS, -Rbar
	1042	On +Vbar, flyaround complete
	1042	Sep-1
	1112	Sep-2	91.26 329 x 343 x 51.6
2008 Feb 20	1026:31	PLBD closed	91.25 329 x 342 x 51.6
	1259:52	OMS DO 2:44 88.4m/s?
	1302:35	OMS DO CO
	1335:30	Entry interface
	1407:09	MGTD KSC RW15
	1407:20	NGTD
	1408:08	WS
	1925	Tow to OPF/1

Making Waves : A PrettyTOUGH Novel

 https://welib.org/md5/a1160b2a9924edcf661e2c42afc5b4db

Manhattan Family Guide To Private Schools And Selective Public Schools

https://welib.org/md5/21b50d45e2345dc02ca7a3caf8d2b5e4