The Influence of Affluence : How the New Rich Are Changing America

 https://welib.org/md5/b4ad7822023bbf7dc1c9e862a9c73d31

All Eyes On Her

 https://welib.org/md5/dd41904490d2d89e1d4dbeece816934d

Turksat 1C

 1996-040B

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Turksat 1C was lauched by Ariane for Aerospatiale, which delivered it on orbit to Turk Telecom. Launch mass was 1743 kg, BOL mass 1078 kg and dry mass 789 kg. The satellite is 1.64 x 1.46 m x 2.20 m with a 22.20 m span. It was built by Aerospatiale-Cannes. The satellite was launched in the lower Ariane position, underneath the SMS (Stretched Mini Spelda) structure. It provides services to Turkey. Initial test position is 31.3E, then service position is 42E.

Turksat 1C
Date	Time	Event	Orbit
1996 Jul 9	2224	Launch by Ariane 44L (V88)	CSG ELA2
	2227	Stage 1 sep T+3:32
	2229	Stage 2 sep T+5:43
	2229	Stage 3 TIG T+5:48
	2242	Stage 3 MECO T+18:45
	2244	Arabsat 2A sep T+20:00
	2246	SMS sep T+22:52
	2248	Turksat sep T+24:20
1996 Jul 11			630.00 212 x 35718 x 7.0
1996 Jul 11	1130?	LAM-1
1996 Jul 11			755.49 6476 x 35722 x 3.4
1996 Jul 12	1230?	LAM-2
1996 Jul 12			1299.66 30345 x 35798 x 0.2
1996 Jul 14	0730?	LAM-3
1996 Jul 14			1434.18 35688 x 35810 x 0.1 GEO 29.9E+0.5E
1996 Jul 20			1435.81 35775 x35786 x 0.1 GEO 31.4E
1996 Jul 22			GEO 31.3E+0.1/d
1996 Aug 6			1436.02 35773 x 35796 x 0.1 GEO 31.3E
1996 Sep 14			1436.00 35769 x 35799 x 0.0 GEO 31.5E
1996 Sep		Move to 42E
1996 Oct 4			1436.07 35773 x 35799 x 0.0 GEO 42.0E
1999 Oct 15			1436.09 35777 x 35795 x 0.0 GEO 42.0E
2006 Aug 1			1436.06 35768 x 35803 x 0.1 GEO 42.0E
2008 Jul 30		GEO 42E, move to 30E
2008 Aug 24			1436.03 35772 x 35798 x 0.4 GEO 31.0E
2010 Jan 29			1436.08 35771 x 35800 x 2.2 GEO 31.0E

December 29,1998

 https://web.archive.org/web/20080504033425/http://digest-archive.degrassi.ca/DD53.htm

January 2000

https://web.archive.org/web/20080504034040/http://digest-archive.degrassi.ca/DD76.htm

https://web.archive.org/web/20080504034054/http://digest-archive.degrassi.ca/DD78.htm

https://web.archive.org/web/20080504034816/http://digest-archive.degrassi.ca/DD80.htm

https://web.archive.org/web/20080504034823/http://digest-archive.degrassi.ca/DD81.htm

https://web.archive.org/web/20080504034830/http://digest-archive.degrassi.ca/DD82.htm

ST-5

 2006-008A

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Each Nanosat Constellation Trailblazer is 25 kg, 0.52m dia 0.48 high oct prism with an extendable boom for 1.0m? span. Three satellites on a single launch to 300 x 4500 km x 97 deg on Pegasus XL from Vandenberg. Built by GSFC. Will study magnetosphere; spacecraft highly magnetically clean to allow short mag booms.

ST5
Date	Time	Event	Orbit
2006 Mar 14	1327	L1011 T/O V RW30/12
	1428	Abort
	1448s	Land on RW12
2006 Mar 22	1304	L1011 T/O V RW30/12
	1403:45	Drop
	1403:50	T+0:05 Stage 1 on 70s
	1405:02	T+1:17 Stage 1 burnout
		Stage 1 sep
	1405:16	T+1:31 Stage 2 on
	1405:55	T+2:10 Fairing sep, 115 km
	1406:29	T+2:44 St 2 burnout, 156 km
	1409:02	T+5:17 Stage 2 sep
	1409:02	T+5:17 Stage 3 burn 283 km
	1410:09?	T+6:24? Stage 3 burnout
	1413:16s	T+9:31 ST5-FWD sep S+0
	1416:26	T+12:41 ST5-2 sep S+200s
	1419:36	T+15:51 ST5-3 sep S+390s	301 x 4568 x 105.6
		Pegasus CCAM
	1532		298 x 4554 x 105.6
2008 Jun 30		end of ops

Payload:

• X-band transponder, Aero Astro comms system

• CULPRIT Low power microelectronic device, CMOS ultra low power radiation tolerant logic.

• Cold gas microthruster, Fine attitude adjustment

• Lithium ion power system

• Magnetometer booms, 0.36m long

Haiyang 3

 2011-043A

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Ocean No. 2 (Haiyang er hao) with CZ-4B. Orbit was 689 x 712 km x 88 deg.

HY2
Date	Time	Event	Orbit
2011 Aug 15	2257	Launch by CZ-4B	TYSC
	2259?	St 1 sep
	2300?	Fairing sep
	2303?	St 2 MECO
	2303?	St 2 sep
		St 3 burn
	2307?	St 3 MECO
	2317?	St 3 sep

Payload:

• MWI Microwave imager, for brightness temp

• RA Dual band radar altimeter C/Ku, sea levels and wind speeds

Skynet 4D

 1998-002A

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Skynet 4D is the first of three replacement Skynet 4 Stage 2 satellites. It will be launched 1998 by Delta. It is built by Matra Marconi Space/Stevenage. It still uses the old ECS bus, but has a steerable high power SHF spot beam and widebeam antennae.

During launch, the Delta second stage suffered two jolts, one during the second burn and one 15 s into the depletion burn, which caused the nearly empty stage to tumble.

The Skynet 4D was transferred from MMS to MoD on 1998 May 20.

In early 2003 4D was moved from the Atlantic position to support troops in the Middle East.

Skynet 4D
Date	Time	Event	Orbit
1998 Jan 10	0032:01	Launch by Delta 7925	CC LC17B
	0033:04	SRM 1-6 burnout
	0033:07	SRM 7-9 burn, 1-6 sep
	0034:10	SRM 7-9 burnout, sep
	0036:24	T+4:23 MECO
	0036:32	T+4:31 Stage 1 sep
	0036:38	T+4:37 Stage 2 burn 324s
	0036:48	T+4:47 Fairing sep
	0042:02	T+10:01 SECO 1	165 x 212 x 29.2
	0053:01	T+21:00 Stage 2 restart 37s
	0053:38	T+21:37 SECO 2	340? x 1140? x 28.6
	0139:29	T+1:07:28 Stage 2 restart 41s
	0140:10	T+1:08:09 SECO 3	1085? x 1372? x 28.6
	0141:53	T+1:09:52 Stage 2 sep
	0142:30	T+1:10:29 Stage 3 burn
	0143:57	T+1:11:56 TECO
	0145:50	T+1:13:49 PAM-D sep
	0145:52	Yo-yo deploy
	0202:00	Stage 2 depletion 25s	764 x 1296 x 26.9
	0202:15	Stage 2 tumble
1998 Jan 10			655.23 1186 x 36036 x 23.7
1998 Jan 12	0225?	AKM burn
1998 Jan 13			1442.75 35690 x 36143 x 4.2 GEO 43.2W+1.6W
1998 Jan 24			1426.77 35560 x 35647 x 4.2 GEO 24.0W+2.3E
1998 Mar 5			1435.96 35753 x 35814 x 4.2 GEO 6.0E
1998 Apr 21			1436.07 35771 x 35800 x 4.0 GEO 6.0E
1998 Apr		Move out
1998 May 5			1430.85 35545 x 35822 x 4.0 GEO 28.7E+1.3E
1998 May 20		Transfer to MoD
1998 Jul 11	Move in	1436.07 35783 x 35788 x 3.9 GEO 53.0E
1999 Jul 28			1436.05 35782 x 35788 x 3.3 GEO 52.9E
1999 Aug 6		move out
1999 Oct 15			1439.78 35781 x 35935 x 3.1 GEO 34.4W+0.9W
1999 Nov 18			1436.12 35779 x 35794 x 3.1 GEO 33.9W
2000 Oct 4			1436.11 35783 x 35789 x 2.5 GEO 34.0W
2002 Oct 26			1436.11 35780 x 35792 x 1.4 GEO 33.9W
2002 Nov 21			1430.52 35559 x 35795 x 1.4
2003 Jan 31		mv in	1436.20 35777 x 35796 x 1.3 GEO 38.9E
2003 Dec 2			1436.02 35779 x 35791 x 1.4 GEO 39.1E
2003 Dec		Move out of GEO
2004 Mar		mv in	1436.16 35775 x 35800 x 1.5 GEO 34.1W
2004 Aug 11			1436.09 35774 x 35799 x 1.7 GEO 34.1W
2006 Jul 30			1436.18 35781 x 35795 x 3.1 GEO 34.4W

UARS

 1991-063B

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The Upper Atmosphere Research Satellite, built by General Electric, used the Fairchild MMS bus (like Landsat D). It had a total mass of 6526 kg at deployment per the SODB; 6540 kg per the press kit. The satellite was launched on STS-48. The RMS grappled the satellite at 2300 on Sep 14, and it was finally deployed at 0423:02 on Sep 15 into a 563 x 574 km x 57.0 deg orbit. Orbit raising burns were made at 1035 on Sep 17 and 1036 on Sep 18.

UARS
Date	Time	Event	Orbit
1991 Sep 14	2300	RMS grapple UARS
1991 Sep 15	0423:02	RMS deploy UARS
1991 Sep 15			563 x 574 x 57.0
1991 Sep 17			563 x 574 x 57.0
1991 Sep 17	1035	orbit raise	555 x 587 x 57.0
1991 Sep 18	1036	orbit raise	574 x 575 x 57.0
1991 Sep 24	0230		574 x 581 x 57.0
1991 Sep 30	1200		574 x 581 x 57.0
1992 Jul		ISAMS failed
1993 May		CLAES cryogen depleted
1999?		End of orbit maintenance
2005 Sep 17			550 x 560 x 57.0
2005 Sep 22?		Begin perigee lower
2005 Oct 5		Burn	507 x 558 x 57.0
2005 Oct 6		Burn	473 x 556 x 57.0
2005 Oct 12		Burn	442 x 555 x 57.0
2005 Oct 18		Burn	415 x 554 x 57.0
2005 Dec 8		Burn
2005 Dec 14	1716	decommissioned
2011 Sep 24	0400	Entry over Pacific 14.1S 170.2W

Payload:

• MMS HPM MMS Hydrazine Propulsion Module, 4 x 5lb thrusters

• MMS MACS MMS Modular Attitude Control System. This unit originally flew on Solar Max, and was returned to Earth by Shuttle Mission 41-C in 1984 for refurbishment.

• SUSIM 2 Solar UV spectral irradiance monitor; 1000-4000A solar spectrum. 2 spectrometers in one instrument.

• CLAES Cryogenic Limb Array Etalon Spectrometer

• ISAMS Improved Stratospheric and mesospheric sounder

• MLS Microwave Limb Sounder, 1.6m reflector, 63, 183 and 205 GHz

Seventeen: April 2011

 https://welib.org/md5/7ba7ad67fa7f22c6203cb5fffbed6c3c