The Go-For-Gold Gymnasts

https://welib.org/md5/d68b06ce902a387eb4500839f9e71e41

Navstar 40

 1996-041A

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SVN 40 was launched in Jul 1996 to replace an older satellite. It was given the ID PRN 10 and placed in slot E3. It was retired in 2015 to be replaced by SVN 72.

Navstar 40
Date	Time	Event	Orbit
1996 Jul 16	0050:00	Launch by Delta 7925	CC LC17A
	0051	GEM 4 to 9 sep
	0051	GEM 1 to 3 ignite
	0052	GEM 1 to 3 sep
	0054:20	T+4:20 MECO
	0054	Thor stage sep
	0054	SES-1
	0100:28	T+10:28 SECO-1
		Delta coast
	0109:51	T+19:51 Delta burn SES-2 19s
	0110:10	SECO-2
	0111:02	T+21:02 Delta sep
	0111:40	PAM-D burn 1:27
	0113:07	TECO
	0115	PAM-D sep
	0143?	Delta depletion	462 x 564 x 35.2
1996 Jul 18	1543	AKM burn
1996 Jul 23			723.65 20275 x 20368 x 55.0
1996 Aug 15		Nav service operational in slot E-3
2015 Jul 16		Decommissioned

It’s a Test

 2017-U01

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Rocket Lab Electron, target orbit 300 x 500 x 83. Payload was instrumentation attached to the second stage.

Electron
Date	Time	Event	Orbit
2017 May 25	0420:00	Launch by Electron	RL LC1
		T+2:34 Stage 1 MECO
		T+2:37 Stage 1 sep
		T+2:41 Stage 2 burn
		T+3:05 Fairing
		T+3:40 St 2 burn still ongoing

STS-117 (Atlantis)

 2007-024A

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STS-117 delivers the S3/S4 truss to the Station. Launch mass is 122515 kg, landing mass 90272 kg. NC2 mass is 115842 kg. Cargo MD to ISS 579 kg plus 799 kg consumables, ISS to MD 693 kg. Deployed 16506 kg. (16183 kg quoted for S3/S4, leaving 323 kg instead of 579 kg expected)

EMU 3010 (EV1 Reilly) and 3004 (EV2 Olivas) on Atlantis, with helmets 1072 and 1068; transfer to ISS, then return.

EMU 3018 for EV3 Forrester, EMU 3006 for EV4 Swanson (aboard ISS) EMU 3008 also on ISS, unused. SAFER 1005 and 1006 to be used; 1003 on ISS out of cert.

 

STS117
Date	Time	Event	Orbit
2007 Feb 7		Tow to VAB
2007 May 15	0902	Rollout to LC39A
2007 Jun 8	2338:04	Launch
	2340:07	T+2:05 SRB sep
	2340:17	T+2:15 OMS assist
	2343:08	T+4:50 OMS assist CO
	2346:29	T+8:30 MECO
	2346:50	T+8:46 ET sep	58 x 220 x 51.6
2007 Jun 9	0016:34	T+38:30 OMS-2
	0017:38	OMS-2 CO	158 x 228 x 51.6
	0052?	ET reentry
	0120:10	PLBD open
	1640:44	OMS 3 NC2 30s
	1641:11	OMS 3 CO
	1751	RMS grapple OBSS
2007 Jun 10	0109:49	OMS 4 NC3
	0111:22	OMS 4 CO
	1527:28	NC4 OMS-5
	1528:19	OMS 5 CO
	1604	NCC
	1700:37	TI OMS6-L 3m/s 12.2s
	1700:49	OMS 6 CO
	1828	Arriving on R-bar nadir
	1848	Begin flyaround from nadir
	1900	+V-bar, begin approach at 120m
	1936:10	Docking
	2058	SRMS grapple S3/S4
	2104	HO to ISS (MCC SR)
	2121	HO to ISS
	2219?	Unberth S3/S4
2007 Jun 11			91.24 329 x 340 x 41.6
		SSRMS at WS2 on end of S1
	0019	SSRMS grapple S3/S4
	0028	SRMS ungrapple S3/S4
	0055	Anderson/Williams IELK transfer
	1750	S3/S4 close to S1
	1803	Ready to latch
	1827	S3/S4 berthed to ISS truss
	1911	3 of 4 bolts complete
	1921	SSRMS ungrapple S3/S4
	1938	Bolts complete
	1947	Airlock at 5 psi
	1951	2.0 psi
	1955	1.2 psi
	2000	Less than 1 psi
	2002	0.5 psi
	2002	HO
	2002	EVA-1 battery power
	2009	Egress Reilly
	2014	Egress Olivas
	2245	Blanket boxes deployed
2007 Jun 12
	0039	Radiator deploy begins
	0050	Radiator deploy complete
	0146	Olivas ingress
	0200	Reilly returning to AL
	0206	Reilly ingress
	0207	TC closed
	0212	HC
	0217	Repress
	1546	SAW S4-1A deploy
	1629	Deploy complete
	1716	SAW S4-3A deploy
	1758	Deploy complete
2007 Jun 13
	0248	MT from WS2 to WS3
		Begin retract of remaining P6 array
	1812	Depress below 2psi
	1814	Depress to 2 psi
	1825	0.5 psi
	1827	HO EVA-2
	1828	Batt power
	1835	Egress Forrester
	1844	Egress Swanson
		Release launch locks on S4
2007 Jun 14
	0124	Ingress Swanson
	0128	Ingress Forrester
	0140	HC
	0144	Repress
2007 Jun 15
		EVA-3 Reilly Olivas
	1720?	Depress
	1724?	HO
	1724	Battery power
	1740?	Egress
	1850	Thermal blanket repair on OMS pod, Olivas
		Reilly installs H vent on Destiny
	1950?	Blanket work complete
	2000	ISS computers reactivated
	2200	Working on P6 retract
2007 Jun 16
	0030	P6 2B SAW fully retracted
	0105?	Ingress Olivas
	0114	Ingress Reilly
	0118	HC
	0122	Repress
	0403	MT from WS3 (S1) to WS5 (S0)
	1428s	SSRMS grapple Lab, ungrapple MBS
	1858s	MT from WS5 to WS1 (S3)
2007 Jun 17
		EVA-4 Forrester, Swanson
		EVA-4: SARJ drive lock assemly ver
		S3 drag link/keel pin stowage
		H vent valve debris shield bolt
		LAN cable from Unity to Zvezda
		SASA gimbal lock release
		2.0 psi
		Depress pump off
	1622?	Depress
	1624	HO
	1625	Battery power
	1632	Egress Forrester
	1638	Egress Swanson
	1700?	Camera stanchion from ESP2
	1718?	VSSA installed on S3 (or P1?)
		S4 SARJ checked out
		MT pathway cleared to S3/S4.
	2211	LAN cable installed, probs w/ MMOD reinstall
	2225	H vent valve opening
	2240?	Ingress Swanson
	2246	Ingress Forrester
	2251	HC
	2254	Repress
2007 Jun 18		ISS crew to ISS; Williams to Atlantis
	2251	HC to ISS
2007 Jun 19
	1442:00	Undocking	91.25 330 x 341 x 51.6
	1446	14m away
	1452	37m away
	1457	61m away
	1506	120m away
	1510	137m away
	1512	On +Vbar, begin flyaround
	1518	152m
	1522	175m on R-bar (above)
	1531	205m
	1534	-V-bar (behind)
	1547	200m below
	1600	195m in front (+V-bar)
	1601	Sep burn at 200m
	1629	Sep burn 2 at 600m?, 0.3m/s
2007 Jun 21	1439	PLBD closed
	1742	PLBD open	91.26 331 x 341 x 51.6
	2045?	RCS phasing burn 5 m/s	91.42 333 x 354 x 51.6
2007 Jun 22
	1434:17	PLBD closed	91.42 333 x 354 x 51.6
	1843:47	OMS DO 2:33 89.3m/s
	1846:21	OMS DO CO	88.35 31? x 354 x 51.6
	1918:13	Entry interface
	1949:38	Landing RW22 EAFB
	1949:48	NGTD
	1950:48	Wheels stop
2007 Jul 1	1304	SCA 905 takeoff from EAFB RW22
	1546?	SCA lands at Amarillo, TX (KAMA)
	1806	SCA 905 takeoff from KAMA
	1946	SCA905 land Offutt AFB
2007 Jul 2	1255	SCA 905 to Ft Campbell
	1435	SCA905 land Ft Campbell
2007 Jul 3	1015	SCA 905 takeoff
	1227	SCA land at KSC SLF RW15
	1630	Tow to OPF/1

Panamsat 1R

 2000-072A

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Ariane 5 launch of HS-702 satellite.

Mass is 4793 kg launch 3000 kg dry. Size 6.2 x 3.5 x 3.3m, 41.0m span.

Launched with AMSAT Phase 3D, the SBS adapter, ASAP-5 with STRV-1c, STRV-1d.

PAS 1R will get to 45W.

PAS 1R
Date	Time	Event	Orbit
2000 Nov 16	0107:00	EPC MES
	0107:07	T+7s Launch of V135
		T+2:25 EAP sep
		T+3:18 Fairing sep
	0116	T+9:40 EPC MECO
	0116	T+9:46 EPC Sep	53 x 1669 x 6.9
	0116	T+9:53 EPS burn
	0133	T+26:53 EPS MECO
	0136	T+29:03 PAS-1R sep
	0141	T+34:05 STRV-1c sep
	0141	T+34:06 STRV-1d sep
	0148	T+41:12s ACU 1663SP/ACY 2624 sep
	0148	T+41:12s SBS sep
	0148	T+41:43s Phase 3D sep
		T+53:35 End of launch phase
			704.12 613 x 39065 x 6.4
	0248?	EPC reentry
2000 Nov 19	1600?	LAM-1	810.98 5704 x 39154 x 2.1
2000 Nov 22	1330?	LAM-2
2000 Nov 24			1138.25 20406 x 39061 x 1.0
2000 Nov 25	1630?	LAM-3
2000 Nov 26			1413.19 31593 x 39080 x 0.2
2000 Dec 4			1436.80 32596 x 39004 x 0.1 GEO 65.5W+0.1W
2000 Dec 19			1436.56 34332 x 37259 x 0.1 GEO 62.5W+0.1W
2001 Feb 27		Move in 45W
2001 Jun 5			1436.15 35786 x 35788 x 0.1 GEO 45.0W
2006 Aug 3			1436.11 35784 x 35789 x 0.1 GEO 45.0W
2009 Dec 18			1436.12 35785 x 35787 x 0.0 GEO 45.0W
2009 Dec 18		Relocate to 50W
2009 Dec 23		Move in
2009 Dec 31			1436.05 35783 x 35788 x 0.1 GEO 50.0W
2012 May 18			1436.09 35775 x 35797 x 0.0 GEO 50.0W
2017 Jan 6			1436.21 35759 x 35818 x 0.0 GEO 50.4W

Hispasat 1C

 2000-007A

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Alcatel/Cannes Spacebus 3000B2 for Hispasat SA, Madrid. 24 Ku-band transponsers. Launch mass 3112 kg at separation. The satellite had three coverage zones: Iberian peninsula - Canary Islands - N Africa; European zone, and N America - Latin America zone.

Hispasat 1C
Date	Time	Event	Orbit
2000 Feb 3	2330	Launch by Atlas IIAS AC-158	CC LC36B
		T+00:57 SRM1-2 burnout
		T+00:59 SRM 3-4 burn
		T+1:06 SRM1-2 sep
		T+1:57 SRM 3-4 sep
		T+2:44 BECO
		T+2:47 Booster sep
		T+3:21 Fairing sep
		T+5:00 SECO
		T+5:02 Atlas sep
		T+5:19 MES1
	2339	T+9:44 MECO1	151 x 373 km x 27.3
		T+24:30 MES-2
		T+26:18 MECO-2
	2358	T+28:56 Centaur sep	166 x 46047 x 18.8
2000 Feb 5			834.22 222 x 45730 x 18.7
2000 Feb 16			1435.99 35768 x 35800 x 0.1 GEO 30.5W
2000 May 25			1436.11 35773 x 35800 x 0.1 GEO 30.1W
2006 Aug 2			1436.11 35770 x 35803 x 0.0 GEO 30.0W
2013 Nov 11			1436.14 35779 x 35795 x 0.1 GEO 30.0W
2013 Nov 21		move out
2013 Dec 30			1440.47 35860 x 35883 x 0.1 GEO 71.4W+1.1W/d
2014 Jan 17		Move in	1436.04 35767 x 35802 x 0.1 GEO 83.8W
2016 Mar 1		Renamed Hispasat 84W-1 (H84W-1)	1436.07 35774 x 35797 x 0.0 GEO 83.9W
2017 May 29			1436.12 35752 x 35822 x 0.5 GEO 83.8W