Navstar 34

 1993-068A

---

Navstar SVN 34 (USA 96) was launched in 1993 Oct 26 by Delta 7925. It was to be retired in 2015.

Navstar 34
Date	Time	Event	Orbit
1993 Oct 26	1704:00	Launch by Delta 7925	CC LC17
	1705	T+1:03 SRM 1-6 off
	1705	T+1:05 SRM 7-9 on
	1705	T+1:06 SRM 1-6 sep
	1706	T+2:09 SRM 7-9 off
	1706	T+2:12 SRM sep
	1708	T+4:20 MECO
	1708	T+4:28 Stage 1 sep
	1708	T+4:34 SES-1
	1708	T+4:44 Fairing sep
	1714	T+10:28 Delta SECO-1	185 x 185 x 34?
	1723 T+19:51 SES-2 19s
	1724	T+20:10 SECO-2	180? x 697? x 34.6?
	1725	T+21:02 Stage 2/3 sep
	1725	T+21:40 TES
	1727	T+23:07 TECO
	1729	T+25 Stage 3 sep	184 x 20382 x 34.86
	1832?	T+1:28? SES-3 depletion	94.45 451 x 532 x 35.2
1993 Oct 28	1338?	Star 37XFP burn	710.45 19849 x 20143 x 55.1
1993 Nov 22		In service
1993 Dec 1		Nav service official
1997 Feb 1		Operating at slot D-4

Clueless: Cher's Guide to Whatever

https://welib.org/md5/f075211bc04384d2e1c3f423d803f809

Spaceflight: November 1996

 https://welib.org/md5/3a4f4bae82b6a23a2bfe277078f847e1

Stable Hearts

 https://welib.org/md5/b881f916ec3b3e126ef4b2bf2de8b8e3

Kosmos 1904

 1987-106A

---

Kosmos-1904,like some other Parus satellites of the time,occasionally provided communications support for the Mir space station whenever its orbital plane allowed.

Kosmos-1904
Date	Time	Event	Orbit
1987 Dec 23	2022:40	Launch by 11K65M	Plesetsk
		T+2:10 St 1 MECO
		T+2:12 St 1 sep
		T+2:12 St 2 burn 59km
		T+2:27 Fairing 76km
	2030?	T+8:03 St 2 MECO 150 km	150 x 1003? x 83
		T+1:02:19 St 2 MES2
		T+1:02:30 St 2 MECO2
	2125?	T+1:02:50 St 2 sep
1988 Jan 15			967x1008x82.9

STS-34 (Atlantis)

 1989-084A

---

The fifth flight of Atlantis was another planetary deployment mission. The Galileo space probe with its IUS booster were mounted on an IUS tilt cradle in the payload bay. Special payload bay modifications handled the cooling of the probe's nuclear RTG power system. Galileo was successfully deployed only six hours after launch, in a 295 x 303 km x 34.3 deg orbit. The major secondary payload on this flight was the Solar Backscatter Ultraviolet experiment to measure the ozone concentration in the upper atmosphere; it was carried in GAS cans on the bay sidewall. The STEX and MLE experiments, IMAX camera and plant and polymer experiments were also carried. Atlantis landed at Edwards on Oct 23.

STS-34
Date	Time	Event	Orbit
1989 Aug 21		Tow to VAB
1989 Aug 29		Rollout	LC39B
1989 Oct 18	1653:40	Launch from LC39B
	1655:44	SRB sep
	1702:12	MECO	72 x 291 x 34.3 (PK)
	1702:30	ET sep	88.22 74 x 298 x 34.3 (OMS dV)
	1733:35	OMS-2 2:21 67m/s
	1735:56	OMS-2 CO
	1821	PLBD open	90.51 295 x 303 x 34.31
	2140	IUS tilt table raised 29 deg
	2315:03	Galileo/IUS deploy
	2330:02	OMS-3 sep burn 17s 9m/s
	2330:19	OMS-3 CO
1989 Oct 19	0223		90.84 299 x 332 x 34.3
1989 Oct 21	0700		90.86 299 x 333 x 34.3
1989 Oct 23	1300	PLBD closed	90.83 297 x 333 x 34.3
	1531:45	OMS DO (2:46) 98 m/s
	1534:31	OMS DO CO	87.49 2 x 296 x 34.3 (OMS dV)
	1602:15	Entry
	1633:01	Landed RW23 EAFB
	1633:11	NGTD
	1634:01	Wheels stop
1989 Oct 28	1445	SCA takeoff	EAFB
	1830	SCA landing	Biggs AAF TX
	2110	SCA takeoff
	2245	SCA landing	Columbus AFB MS
1989 Oct 29	1900	SCA takeoff	Columbus AFB MS
	2305	SCA landing	KSC SLF
1989 Oct 30	0150	Tow to OPF/1

Resurs 48

 1991-052A

---

Resurs F-1 14F43 No. 53 was launched in Jul 1991 carrying the Priroda 4 payload of KFA-1000 long focus cameras and KATE-200 topographic cameras.

Resurs F-1 14F43 No. 53
Date	Time	Event	Orbit
1991 Jul 23	0905	Launch by Soyuz-U	PL LC43/3
	0913	Blok-I sep	88.65 182 x 233 x 82.33
1991 Jul 24	0230	Orbit raise	89.81 257 x 272 x 82.33
1991 Jul 30	0230		89.72 255 x 266 x 82.33
1991 Jul 31	0230		89.82 257 x 273 x 82.33
1991 Aug 6	1200		89.76 254 x 270 x 82.33
1991 Aug 7	1430		89.75 254 x 270 x 82.33
1991 Aug 8
	0450?	Deorbit
	0502?	PO sep
	0514?	Entry
	0529?	Landed

STS-51-J (Atlantis)

 1985-092A

---

The first mission of Atlantis left pad 39A on Oct 3, 1985. Mission 51-J was a classified Department of Defense mission and few details were released at the time. The main payload was a pair of DSCS III military communications satellites mounted on a single IUS solid booster. The payload was deployed early on Oct 4; Atlantis backed away and the IUS first stage fired an hour later. Atlantis remained in orbit for three more days, landing at Edwards on Oct 7. The crew carried out a number of mid-deck experiments for the Space Test Program. 

STS 51-J
Date	Time	Event	Orbit
1985 Apr 6		Rollout	Rockwell Palmdale
1985 Apr 9		Tow to EAFB
1985 Apr 12		SCA takeoff	EAFB
		SCA landing	Ellington AFB TX
1985 Apr 13		SCA takeoff	Ellington AFB
		SCA landing	KSC SLF
1985 Apr 14		Tow to OPF	OPF/1
1985 May 10		Storage	VAB/2
1985 May 28		Tow to OPF	OPF/2
1985 Jun 18		Storage	VAB/2
1985 Jul 13		Tow to OPF	OPF/1
1985 Aug 12		Tow to VAB	VAB/3
1985 Aug 12		ET mate
1985 Aug 30		Rollout	LC39A
1985 Sep 12	1950	FRF (0:20)	LC39A
1985 Oct 3	1515:30	Launch from KSC LC39A
	1517:34	SRB sep
	1524:02	MECO
	1524:20	ET sep	? 60? x 470? x 28.5
	1557:55	OMS 2	94.05 469 x 476 x 28.5
	1602:07	OMS 2 CO
	1638	ET-25 breakup at 65 km
	1648:19	PLBD open
	2111		94.07 470 x 476 x 28.5
1985 Oct 4	0148?	DSCS/IUS deploy
	0203:24	OMS-3 sep
	0203:45	OMS-3 CO
	0203		94.53 475 x 515 x 28.5
1985 Oct 5			94.53 476 x 515 x 28.5
1985 Oct 7	0500	94.55 478 x 515 x 28.5
	1228:49	PLBD L close
	1322:31	PLBD R close
	1600:37	OMS deorbit
	1630:21	Entry interface
	1700:08	Landed RW23 EAFB
	1700:15	NGTD
	1701:13	Wheels stop
1985 Oct 11	1355	SCA takeoff	EAFB
	1625	SCA landing	Kelly AFB TX
	1845	SCA takeoff
	2210	SCA landing	KSC SLF
1985 Oct 12	0250	Tow to OPF/1

Kosmos 395

  1971-013A

---

Kosmos-395,a Tselina-O ferret satellite, was launched in Feb 1971 and entered a 95.4 minute orbit.

Kosmos-395
Date	Time	Event	Orbit
1971 Feb 17	2104?	Launch by 11K65M	PL
	2106?	Stage 2 burn
	2115?	Stage 2 coast
	2140?	Stage 2 burn 2
	2140?	Stage 2 sep
1971 Mar 2	0700		95.41 529 x 546 x 74.04
1980 Apr 6		Reentered

Luna 13

  1966-116A

---

Following the successful missions of the lunar orbiter E-6S and E-6LF craft, a final E-6M, No. 205, was sent aloft as Luna-13, and repeated the landing achieved by Luna-9. The spacecraft was originally No. 14, developed by OKB-1.

Luna-13
Date	Time	Event	Orbit
1966 Dec 21	1017	Launch by Molniya	KB
	1022	Blok-A sep
	1022	Blok-I burn
	1026	Blok-I sep
	1117?	BOZ burn
	1118?	Blok-L burn
	1122?	Blok-L sep
1966 Dec 22	1841	TCM
1966 Dec 24	1759	Modules sep
	1759	Retro burn 70 km
	1800	DU sep
	1801	Landed on Moon 18 52N 62 03 W
	1805	Petals unfold
	1806	Soil penetrator test
1966 Dec 26		Additional imaging
1966 Dec 28		End of transmissions

Polyus

 1987-U01

---

The first launch of the Energiya booster carried a 100 tonne spacecraft, 17F19DM Skif-DM, which was a prototype of the Polyus (pole) station. Skif-DM was built around a TKS-type FSB (Funktsional'no-sluzhebnovo blok, Operations/service Unit), No. 162, with an enormous payload section carrying a mockup prototype laser weapon.

The Polyus was 37.57 m long and 4.1m in diameter, with a planned in orbit mass of 88 tonnes. It may have included a set of subsatellites which were to have been used for a missile defense sensor technology experiment, similar to the US Delta 181 mission,  although these may have been cancelled prior to launch.

Launch was at 2130 Moscow Time. Energia No. 6SL launch mass was 2365 tonnes. The Blok A strapons carried 1240t fuel, Blok Ts carried 710t fuel, Blok A dry was 250t, Blok Ts was 86t, leaving 80t for the payload.

After separation of Skif-DM from Energiya, Skif began a planned 180 degree rotation. The rotation should have been stopped at 180 degrees but was not; the DKS engines fired at apogee while Skif completed two whole revolutiions in pitch. The engines should have changed the orbit by 87 m/s to a 155 x 280 km orbit; a second burn at 1830 UTC would have circularized the orbit at 280 x 280 km x 64.6 deg.

Skif-DM
Date	Time	Event	Orbit
1987 May 15	1730:01	Launch by Energiya 6SL	KB
		T-14.4s Blok Ts MES
		T-3.2s Blok A (1-4) MES
		Zenit strapons sep
	1733	T+3:32 GO (fairing) sep, 2 sections, 90 km
	1737	T+7:36 Energiya core to low thrust
	T+7:39 Energiya engines cutoff
	1737	T+7:40 Energiya/Skif-DM sep at 110 km	-15 x 155 x 64.61
	1738	T+8:32 Skif-DM orientation mvr begins
	1739	T+9:25 DO (Donnovo obtekatel') sep
	1739	T+9:28 BB Side fairings sep (2?), SBV exhaust cover sep
	1739:29	T+9:28 Polyus ODU burn, 384s 87m/s
	1745	T+15:25 Apogee 155 km; DKS burn fires in wrong direction
	1822	T+52:07 Polyus impact in Pacific

Aviation Week: December 16,1996

 https://welib.org/md5/79e65f52e291ba91bd760242143e96f8

Raduga 23

 1989-048A

---

The first Raduga-1 satellite was launched on 1989 Jun 21.

Raduga-1
Date	Time	Event	Orbit
1989 Jun 21	2335:00	Launch by Proton-K	KB
	2344	Stage 3 sep	188 x 197 x 51.6
1989 Jun 22	0052?	DM burn 1 T+1:17
	0615?	DM burn 2
	0619?	DM sep
1989 Jun 22			1474.87 36483 x 36601 x 1.5 GEO 84.2E+9.5W
1989 Jun 27			1456.27 36137 x 36223 x 1.5 GEO 46.1E+5.0W
1989 Jul 1			1436.23 35765 x 35813 x 1.5 GEO 49.3E
1989 Jul 17			1436.17 35764 x 35811 x 1.4 GEO 48.8E
1990 Apr 18			1435.91 35770 x 35795 x 0.7 GEO 49.4E
1991 Feb 2			1436.11 35782 x 35791 x 0.1 GEO 48.7E
1992 Feb 8			1435.93 35774 x 35792 x 0.9 GEO 48.9E
1992 Feb 9		mv out
1992 Mar 11		mv in
1992 Mar 20			1436.24 35785 x 35703 x 1.0 GEO 70.0E
1992 Dec 18			1436.16 35774 x 35801 x 1.7 GEO 69.9E
1994 Feb 13			1436.08 35774 x 35797 x 2.6 GEO 69.5E
1995 Aug 12			1436.07 35770 x 35801 x 3.8 GEO 69.8E
1996 Dec 20			1436.07 35772 x 35799 x 4.7 GEO 69.8E

Aviation Week: March 24,1997

 https://welib.org/md5/5574f0f6fb74ca9d6768f884948796a0

Town and Country: November 1996

 https://welib.org/md5/ffe11ea1503585450148121d57f4fb7a

Aviation Week:December 9,1996

 https://welib.org/md5/610eaa69f96520731b4a01a36aa4386d

Teen: March 1997

 https://welib.org/md5/d3f1f258581c4bc60a70d3d4a307dd4f

Navstar 42

 1997-F01

---

The first 2R satellite (SVN 42, IIR production no 2, PRN 12) was destroyed seconds after liftoff. Mass was 2032 kg. It would have been PRN 12 at slot F5.

Photos showed smoke escaping from the No. 2 solid rocket motor (S/N K-404) followed by fire at the base of the motor and detonation of the entire vehicle. As onlookers raced for cover, fiery debris rained down on complex 17. The investigation found that the SRM split along its length, with the split propagating forward prior to complete failure at 12 seconds when the vehicle first stage self-destruct activated. The RSO sent destruct at 22 seconds, destroying the second and third stages. The payload and fairing were destroyed on impact with the ground. The PAM-D left an 8-m dia crater. It was concluded the SRM had been damaged at some point prior to launch.

GPS 2R No. 2
Date	Time	Event	Orbit
1997 Jan 17	1628:00	Launch by Delta 7925	CC LC17A
	1628:02	Telemetry interruption (T+2s)
	1628:07	SRB No 2 (K-404) burnthrough (T+7s)
	1628:13	SRB exploded (T+13s) alt 0.48 km
	1628:13	Vehicle exploded (self-destruct) T+12.6s
	1628:22	RSO destruct sent (T+22.3s)
	1628	Debris impact LC17A

Kosmos 1585

 1984-077A

---

TLEs are missing for the first week of flight,but the orbit has been reconstructed from various observations. A TG beacon was detected throughout the flight.

Kosmos-1585
Date	Time	Event	Orbit
1984 Jul 31	1229:54	Launch by Soyuz	KB
	1238?	Blok I sep
1984 Jul 31			181x324x65
1984 Aug 6			89.28 168 x 309 x 64.7
1984 Aug 11			88.88 162 x 275 x 64.7
1984 Aug 11		Orbit raise	89.55 162 x 344 x 64.7
1984 Aug 16			89.17 158 x 307 x 64.7
1984 Aug 16		Orbit raise	89.55 172 x 331 x 64.7
1984 Aug 24			89.08 166 x 291 x 64.7
1984 Aug 24		Orbit raise	89.56 172 x 333 x 64.7
1984 Aug 30			89.21 167 x 303 x 64.7
1984 Aug 31		Orbit raise	89.92 180 x 360 x 64.7
1984 Sep 5			89.68 179 x 338 x 64.7
		Orbit lower	89.14 173 x 290 x 64.7
1984 Sep 7			88.96 171 x 274 x 64.7
1984 Sep 7		Orbit raise	89.55 173 x 330 x 64.7
1984 Sep 12			89.31 171 x 308 x 64.7
1984 Sep 13		orbit raise	89.77 183 x 343 x 64.7
1984 Sep 25			89.13 176 x 286 x 64.7
1984 Sep 26		Orbit raise	89.57 175 x 330 x 64.7
1984 Sep 28			89.45 174 x 320 x 64.7
1984 Sep 29
	1910?	Deorbit
	1924?	Entry
	1936?	Landed

Booklist: March 1,1997

 https://welib.org/md5/404601b3fb06aa71cb595a46b22154dd

Kosmos 1776

 1986-067A

---

Four low RCS objects were released by Kosmos-1776 prior to the start of releases of the 0.2 sq m objects.

Kosmos-1776
Date	Time	Event	Orbit
1986 Sep 3	0900:00	Launch by 11K65M	PL
	0908	Stage 2 MECO-1
	0933?	Stage 2 MECO-2
1986 Sep 3			(67B) 465x516x74.0
1986 Sep 3			473x516x74.0
1986 Oct 8		release 67C-67F (4f)
1986 Dec 24		release 67G-67K (4f)
1987 Jan 27		release 67L,M (2f)
1989 Dec 15		reentered

No	Object	RCS	Release (approx)	Decay
	Kosmos-1776	28.1		1989 Dec 15
	S3 rocket	20.1		1989 Oct 26
S1	C	0.01	1986 Oct 6	1987 Oct 30
S2	D	0.02	1986 Oct 6	1987 Oct 14
S3	E	0.02	1986 Oct 6	1987 Nov 8
S4	F	0.01	1986 Oct 6	1987 Oct 24
1	G	0.22	1986 Dec 24	1987 Dec 9
2	H	0.28	1986 Dec 24	1987 Nov 29
3	J	0.23	1986 Dec 24	1987 Nov 23
4	K	0.17	1986 Dec 24	1987 Nov 14
5	L	0.23	1987 Jan 27	1987 Dec 4
6	M	0.19	1987 Jan 27	1987 Nov 9
7	N	0.17	1987 Jan 27	1987 Dec 27
8	P	0.17	1987 Jan 27	1987 Nov 22
9	Q	0.18	1987 Feb 23	1987 Nov 24
10	R	0.24	1987 Feb 23	1987 Dec 28
11	S	0.25	1987 Jun 2	1988 Jan 13
12	T		1987 Jun 2	1988 Feb 7
13	U	50.1	1987 Oct 22	1988 Sep 20
14	V	0.16	1987 Oct 22	1988 Sep 14
15	W	0.24	1988 Feb 10	1988 May 28
16	X	0.24	1988 Feb 10	1988 Jun 13
17	Y	0.24	1988 Aug 10	1988 Oct 18
18	Z	0.23	1988 Aug 10	1988 Oct 1
19	AA	0.19	1988 Aug 23	1988 Oct 20
20	AB	0.22	1988 Aug 23	1988 Oct 10
21	AC		1988 Sep 29	1988 Nov 8
22	AD		1988 Sep 29	1988 Oct 31
23	AE	2.45	1989 Oct 2	1989 Oct 5

STS-49 (Endeavour)

 1992-026A

---

Endeavour left the pad for the first time on 1992 May 7. On May 10, Endeavour completed its first rendezvous with the Intelsat satellite. Thout and Hieb left the airlock at 2039, and by 2153 Endeavour was stationkeeping with the target. Thout contacted Intelsat with the Capture Bar at 2157:04, but failed to grapple it and the satellite started coning. Brandenstein flew Endeavour toward the satellite again at 2208, and again at 2214, with Thout making a total of 4 contacts. At 2228 the rendezvous was abandoned, with a sep burn half an hour later, and the astronauts reentered the cabin at 0008, closed the hatch at 0012, and repressurized the airlock at 0016 after 3h 51m.

On May 11 at 2102, Endeavour was approaching Intelsat for the second time as Thuot and Hieb depressurized the airlock again, entering the bay at 2107. At 2318 Thout placed the capture bar against the Intelsat, but no grapple ensued. Four more contacts were unsuccessful and once again the rendezvous was abandoned. At 0228 Thout and Hieb, temporarily defeated, repressurized the airlock.

The third try on May 13 began with the airlock depressurized to 5 psi at 1912. The Transfer Initiate (TI) burn to begin the third rendezvous was at 2058 following a one orbit delay because of a software problem. The airlock was depressurized completely at 2109 and the hatch opened at 2112, with three astronauts emerging into open space for the first time. Thuot, Hieb and Akers completed assembly of the lower plane of the ASEM structure by 2219 as Brandenstein began braking the Orbiter.

Akers stood on the ASEM structure, Hieb on the starboard payload bay sill, and Thuot on the PAD foot restraint attached to the RMS arm. The Orbiter remained motionless beneath Intelsat as the astronauts watched it rotate between them. At last, a few seconds before midnight UT, the three astronauts grabbed hold of the errant satellite. They held it motionless for 45 minutes, and then Thuot was moved slightly on the RMS to allow Hieb and Thuot to begin attaching the capture bar. They finally got the bar attached at 0122:57 and hard docked at 0132:55. At 0137 Thuot stepped off hte RMS and Melnick used the arm to grapple the capture bar at 0147. The RMS then moved the Intelsat and capture bar over to the Orbus kick motor. At 0300 the satellite was firmly attached to Orbus. Akers, his consumables running low, moved back to the airlock at 0347.

At around 0415 the grapple extensions on the capture bar were removed, and by 0424 the Orbus motor was electrically connected to the satellite. The RMS was back in its cradle at 0428, and by 0432 all the astronauts were back in the vicinity of the airlock. Thornton gave the command to redeploy the satellite at 0440, but nothing happened. After two further failures, an electrical reconfiguration fixed the problem and at 0453 the Intelsat VI F-3, with its new Orbus 21S kick motor attached, glided out of the payload bay. Hieb reentered the bay for EVA cleanup while two sep burns were made.

At 0541 the three astronauts began repressurizing the airlock; the repressurization was almost complete by 0551. The EVA had lasted 8h 29m. The main goal of the mission achieved, attention now switched to the fourth and final EVA. The hatch opened at 2107 as Thornton and Akers entered the bay. The astronauts constructed the ASEM pyramid, a 4.5m high structure meant to simulate part of the Space Station Truss. Akers also evaluated the Crew Propulsive Device, a hand held gas-powered maneuvering unit. Next, a "leg" was attached to the MPESS pallet, and the RMS arm grappled and unberthed the entire MPESS, which was then attached to the ASEM pyramid. After the MPESS was undocked from the ASEM, the astronauts removed the "leg" and the MPESS was reberthed. The RMS was used to make a photo survey of the latches used to lock down the MPESS, and the ASEM was disassembled (with the base plane left in place). The astronauts returned to the airlock at 0437 and the hatch was closed at 0444. Repressurization was at 0452 after a 7h 45m EVA.

As well as the CPD, STS-49 carried a set of four further devices as part of the CSR (Crew Self Rescue) experiment: the Astrorope, the Bistem Pole, the Inflatable Pole, and the Telescope Pole. However, the extra time taken for Intelsat Rescue operations meant that none of these could be tested.

STS-49
Date	Time	Event	Orbit
1991 Apr 25		Rollout	Palmdale
1991 May 3		SCA takeoff	Palmdale
		SCA landing	Biggs AAF, TX
1991 May 5		SCA takeoff
		SCA landing	Kelly AFB TX
1991 May 6		SCA takeoff
		SCA landing	Ellington Field, TX
		SCA takeoff
		SCA landing	Columbus AFB, MS
1991 May 7		SCA takeoff
		SCA landing	KSC SLF
1991 May 8		Tow to VAB/2	VAB/2
1991 Jul 26		Tow to OPF	OPF/1
1992 Mar 7		Tow to VAB	VAB
1992 Mar		ET mate	VAB
1992 Mar 13		Rollout	LC39B
1992 Apr 6	1513	FRF (0:22)	LC39B
1992 May 7	2340:00	Launch	LC39B
	2342:07	SRB sep
	2348:29	MECO	88.50 63 x 337 x 28.3 (OMS dV)
	2348:48	ET-43 sep	59 x 330 x 28.3
1992 May 8	0019:58	OMS 2 2:04 59m/s	90.53 263 x 337 x 28.3
	0022:02	OMS 2 CO
	0053		90.49 258 x 339 x 28.3
	0115	PLBD open
	0452:44	OMS 3 (LH 16s) 4m/s	90.67 278 x 336 x 28.3
	0453:00	OMS 3 CO
	2045:12	OMS 4 (RH, 18s) 4m/s	90.83 278 x 351 x 28.33
	2045:30	OMS 4 CO
1992 May 9	0500?	RCS burn, NC2
	0824		90.79 275 x 350 x 28.3
	1800	RMS survey, DTO 325
	2011:01	OMS 5 NSR (46s) 22m/s
	2011:47	OMS 5 CO
	2039		91.54 347 x 353 x 28.33
	2117:40	OMS 6 NPC (RH, 12s) 3m/s
	2117:52	OMS 6 CO
	2139		91.57 349 x 352 x 28.33
1992 May 10	0409		91.57 349 x 352 x 28.31
	0419		91.60 352 x 353 x 28.31
	1542:50	OMS 7 L 18s 4m/s
	1543:09	OMS 7 CO
	1730?	Planar null NH2 burn
	1835	NCC
	1933	TI
	1942	RMS power up
	2004	In AL
	2017	Begin AL depress
	2023	MC2
	2022	EVA-1 Depress complete?
	2025	EVA-1 depress
	2025	HO
	2033	MC3
	2039	EVA-1 egress
	2112	On V-bar, rendezvous
	2157	Failed capture	91.87 364 x 367 x 28.31
	2300?	RCS sep
	2327	PLB cleanup
1992 May 11	0008	Ingress
	0012?	HC
	0016	EVA-1 repress
	0016		91.90 365 x 369 x 28.31
		Phasing burn
	0450		91.86 361 x 370 x 28.31
	1658:07	NCC OMS 8 L 9s 2m/s
	1658:16	OMS 8 CO
	2002	TI 2m/s
	2006	AL inner hatch closed
	2030	Begin depress
	2053	At zero pressure EVA-2
	2100	NC3
	2102	EVA-2 depress
	2110	NC4 burn	91.83 358 x 370 x 28.31
	2115	EVA crew gathering tethers
	2127	Preparing capture bar
	2145	Range 50m
	2200	Flyaround Intelsat
	2217	(Re?-)Egress airlock
	2220	Stationkeeping
	2253	Final approach
	2305	Failed to contact Intelsat
	2312	Back off
	2315	Reapproach
	2318:24	Contact Intelsat
1992 May 12	0016	Reapproach
	0028	Contact Intelsat
	0032	Contact Intelsat
	0042	Contact Intelsat
	0100	Contact Intelsat
	0136	PLB cleanup, working on cap. bar
	0139	Ingress?
	0145	RCS sep
	0149	RCS sep	91.85 359 x 370 x 28.31
	0225	Ingress?
	0228	Ingress, EVA-2 repress
	0231	Repress (STSMR)
	0301	Repress cabin
	1717?	NC7 RCS
	1719		91.79 355 x 369 x 28.3
	2100	Test of 3 crew in airlock
	2202		91.78 353 x 370 x 28.3
1992 May 13
	1225	NC8 RCS
	1536?	RCS adjust
	1621	NC9 RCS phasing	91.79 354 x 369 x 28.3
	1829?	RCS NCC
	1830	TI convergence failed
	1929	TI delay
	1930	Airlock at 5 psi?
	2057:55	TI
	2109	EVA-3 depress
	2110	EVA-3 HO (STSMR)
	2109	Depress complete
	2112	Battery power
	2119:37	MC1
	2147	In bay attaching tether reel to arm
	2153:49	MC2
	2203:49	MC3
	2213:49	MC4
	2219	Braking
	2300	Working with capture bar
	2315	Stationkeeping
	2359:31	Manual 3-astro capture of Intelsat VI F-3
1992 May 14	0100?	Capture bar attached to Intelsat by Hieb
	0124	Soft dock (of CB to Intelsat?)
	0133	Hard dock at both ends
1992 May 14	0147:41	RMS grapple CB/Intelsat	91.79 355 x 369 x 28.31
	0207	At PFR for shower cap removal?
	0224	Removed shower cap from Orbus
	0258	Berthing on Orbus
	0300	RMS berth Intelsat on Orbus
	0300	RMS ungrapple Intelsat
	0351	Stowing extension beams
	0354	PAD stowed
	0424?	Head for airlock
	0440	First deploy command, failed
	0453:22	Intelsat deploy
	0516	RCS Sep-1
	0539:22	OMS-9R Sep-2 19s 5m/s
	0539:42	OMS-9 CO
	0536	HC
	0541	EVA-3 repress	91.60 344 x 361 x 28.31
		EVA-4 for ASEM
	2054	Begin depress
	2104?	Depress
	2104	HO
	2107	EVA-4 begin; assemble ASEM
	2107?	EV3 suit problem
	2130?	Egress
	2203?	Begin ASEM assembly
	2306	ASEM assembly complete
	2310?	CPD flight by Akers
	2312?	RMS grapple MPESS
	2318?	RMS unberth MPESS
	2339	CPD experiment completed
1992 May 15	0027?	Beginning attachment of MPESS to ASEM
	0033	Soft dock MPESS/ASEM
	0040	Attach ASEM 'legs' to MPESS
1992 May 15	0110?	RMS docked MPESS to ASEM
	0210	Removing legs
	0241	RMS reberthed MPESS
	0245	RMS ungrapple MPESS
	0310	Disassemble ASEM pyramid
	0340	PLB cleanup
	0434	Ingress
	0440	RMS stowed
	0440	TC closed
	0445?	HC
	0450	Power to SCU
	0452	EVA-4 repress 7:45
1992 May 16	1400		91.58 343 x 361 x 28.32
	1734	PLBD close
	1955:15	OMS DO 2:48 96m/s
	1958:02	OMS DO CO
	2027:03	Entry
	2057:21	Gear down
	2057:38	Landing	RW22 EAFB
	2057:50	NGTD
	2057:51	Drag chute out
	2058:36	Wheels stop
1992 May 27	1945	SCA 911 takeoff	EAFB
1992 May 28	0230	SCA 911 landing	Biggs AAF TX
1992 May 29	1730	SCA 911 takeoff
	1850	SCA 911 landing	Kelly AFB TX
1992 May 30	1030	SCA 911 takeoff
	1450	SCA 911 landing	KSC SLF
	1615	Tow to OPF