TeamNathanFTW’s New and Improved Blog : May 1999

Sunday, May 30, 1999

ATS 6

1974-039A

ATS F (Applications Technology Satellite 6) was the last of the ATS satellites, and a completely different design. Built by Fairchild Industries, the satellite was dominated by its huge, 9.1-meter, 87 kg deployable antenna. The main experiment payload was in the 1.37 m dia Earth Viewing Module (EVM), a box located at the antenna focus.

The Titan IIIC launch vehicle left pad 40 at Cape Canaveral at 1300 UT on 1974 May 30. After solid motor and stage 1 separation, Titan core stage 2 ignited at 1304:16 and entered a 154 x 314 km x 28.6 deg parking orbit. The Transtage and its payload separated from the Titan, and Transtage made its first burn at 1412:26 until 1417:37, into a geostationary transfer orbit. The second Transtage burn to circularize the orbit at geostationary altitude was at 1936:56, and the Transtage separated from ATS 6 at 1941:37. Antenna deployment took from 1947 to 2010 UT.

After braking burns on Jun 6 and Jun 7, the spacecraft reached station at 94 deg W. On 1975 May 30 at 0030, ATS 6 burned to move out of GEO and began the move to 35 deg E for the SITE (Satellite Instructional TV Experiment) in India. Orbit corrections were made on May 21 and Jun 21, and braking burns on Jun 25 and Jun 29. By Jun 30 ATS 6 was on station again and SITE could begin, bringing educational TV to remote villages in India. The experiment lasted one year, and on 1976 Aug 1 ATS 6 moved out of GEO again to head for 140 deg W. Course corrections were made on Aug 4, Nov 29 and Nov 30. A final braking maneuver on 1976 Dec 2 signalled the satellite's arrival at the new position.

Operations at 140W continued until 1979 Jun 30; on Jul 31 a 28 hr long burn lowered the orbit, and on Aug 2 the propellant was burned to depletion, leaving the satellite in a 35224 x 35430 km orbit with a period of 1412.5 min. ATS 6 was switched off at 0144 on Aug 30, but switched on again in 1979 Nov for collection of particle data. The satellite was finally retired in Feb 1980.

Date	Time	Event	Orbit

ATS 6



1974 May 30	1300:00	Launch by Titan 3C
	1301:49	T+1:49 St 1 burn
	1302:01	SRM sep
	1304:17	Stage 1 sep
	1304:16	Stage 2 burn
	1305:05	Fairing sep
	1307:44	T+7:44 Stage 2 MECO	154 x 314 x 28.6
	1308:00	Stage 2 sep
	1412:26	T+1:12:26 Transtage burn 1
	1417:37	T+1:17:37 Transtage MECO1	489? x 35700? x 26.4
	1926:50	Transtage burn 2
	1928:39	Transtage MECO2
	1933:21	Sep
	1938:25	Transtage sep
	1947	Begin antenna deploy
	2008	T+7:08:44 Transtage retro burn
	2010	Complete deploy	35761 x 35817 x 1.78 GEO 94.41W
1974 Jun 6		Braking
1974 Jun 7		Braking	GEO 94W
1974 Jul 1			GEO 94 W
1974 Aug 8		TCM
1974 Sep 14		TCM
1974 Oct 19		TCM
1974 Dec 28		TCM
1975 Feb 22		TCM
1975 May 19			GEO 94W
1975 May 20	0030	Mv out
1975 May 21		TCM
1975 May 25		76W+3E/d
1975 Apr 11		TCM
1975 Jun 21		TCM
1975 Jun 25		braking
1975 Jun 29		braking
1975 Jun 30		SITE, on station	GEO 35E
1975 Jul 3		TCM
1975 Aug 3		TCM
1975 Aug 31		TCM
1975 Sep 28		TCM
1975 Oct 25		TCM
1975 Nov 22		TCM
1975 Dec 20		TCM
1975 Dec 30			GEO 35E (Morgan)
1976 Jan 18		TCM
1976 Jan 31		TCM
1976 Feb 21		TCM
1976 Mar 21		TCM
1976 Apr 18		TCM
1976 May 14		TCM
1976 May 30		TCM
1976 Jun 13		TCM
1976 Jul 11		TCM
1976 Jul 31			GEO 35E
1976 Aug 1		mv out	GEO 35E
1976 Aug 4		TCM
1976 Nov 29		TCM
1976 Nov 30		TCM
1976 Dec 2		Braking, 140W
1976 Dec 12		TCM
1976 Dec 13			GEO 140W
1977 Jan 9		TCM
1977 Jan 20			1436.11 35779 x 35794 x 0.4 GEO 140.0W
1977 Feb 1		TCM
1977 Feb 20		TCM
1977 Apr 6		TCM
1977 May 3		TCM
1977 Jun 7		TCM
1977 Jul 15		TCM
1977 Aug 18		TCM
1977 Sep 12		TCM
1977 Oct 12		TCM
1977 Nov 7		TCM
1977 Dec 9		TCM
1978 Jan 6			1436.01 35770 x 35799 x 1.1 GEO 140.2W
1978 Jan 11		TCM
1978 Feb 15		TCM
1978 Mar 17		TCM
1978 Apr 14		TCM
1978 May 11		TCM	1436.22 35773 x 35804 x 1.4 GEO 140.0W
1978 Jun 7		TCM
1978 Jul 6		TCM
1978 Aug 2		TCM
1978 Aug 24		TCM
1978 Sep 27		TCM
1978 Oct 5		TCM
1978 Oct			GEO 140W
1978 Oct 11		TCM
1978 Nov 8		TCM
1978 Dec 6		TCM
1979 Jan 3			1436.06 35772 x 35799 x 1.9 GEO 140.1W
1979 Jan 4		TCM
1979 Jan 28		TCM
1979 Feb 28		TCM
1979 Mar 28		TCM
1979 May 9		TCM
1979 Jun 6			1436.03 35774 x 35796 x 2.2 GEO 140.0W
1979 Jun 21			1435.94 35772 x 35794 x 2.2 GEO 139.5W+0.03
1979 Jun 30		End of ops	GEO 140W
1979 Jul 9			1435.84 35765 x 35797 x 2.2 GEO 138.6W+0.06W
1979 Jul 31			1435.71 35761 x 35796 x 2.3 GEO 136.8W+0.09W
1979 Jul 31		Test burn
1979 Aug 2		Depletion burn	1412.5 35224 x 35430 x 2.3
1979 Sep 9			1412.03 35190 x 35437 x 2.4
1982 Feb 12			1412.07 35168 x 35461 x 4.2
1990 Jun 1			1411.99 35188 x 35438 x 10.7
1994 Apr 20			1412.04 35168 x 35460 x 13.3
1998 Jul 30			1411.97 35204 x 35421 x 14.7

Aviation Week: January 25,1999

https://welib.org/md5/45a2b74d1f71169e08fb867f141fb975

Friday, May 28, 1999

Town and Country: February 1999

https://welib.org/md5/bc6370814a73d59445622bdec8234585

Aussat 1

1985-076B

The Aussat satellites were owned by the company Aussat Pty. of Australia; three HS376 satellites were built for the project to provide Australian domestic satellite communications. Aussat carried 15 Ku-band transponders, whose direct broadcast capacity was used by the Australian Broadcasting Co. (ABC).

The Aussat K1 apogee burn left it in a 1284 min orbit; a burn the next day raised the orbit to 1318 min and then on Sep 1 to 1421 min, in the geostationary ring. Archival elements for early 1993 are double valued, one subset remaining at 160E and another subset moving to 164E and staying there for several months. The orbit was raised in mid 1993.

Date	Time	Event	Orbit

Aussat K1



1985 Aug 27	1733	PAM-D launch from Discovery, LEO
	1818?	PAM-D burn
	1819?	PAM-D burnout
	1821?	PAM-D sep
1985 Aug 28			651.56 754 x 36281 x 24.4
1985 Aug 30	0552:18	Star 30BP burn
1985 Aug 30			1284.59 29254 x 36278 x 0.9
1985 Aug 31	0320?	mv
1985 Aug 31			1318.70 30644 x 36268 x 0.8 GEO 146.3E+32.1E
1985 Sep 1	0100?	mv
1985 Sep 1			1421.03 35023 x 35958 x 0.2 GEO 162.1E+3.8E
1985 Sep 2		mv in
1985 Sep 3			1436.02 35606 x 35964 x 0.1 GEO 162.4E
1985 Oct 1			1436.18 35781 x 35795 x 0.0 GEO 160.0E
1985 Oct 1		Into service
1986 Sep			GEO 160E
1987 May 16			1436.10 35775 x 35797 x 0.0 GEO 160.0E
1990 May 25			1436.11 35778 x 35795 x 0.0 GEO 160.0E
1992 Jan 28			1436.10 35781 x 35791 x 0.0 GEO 160.0E
1993 Jan 5			1436.09 35775 x 35797 x 0.0 GEO 160.0E

Thursday, May 27, 1999

Milstar 3

1999-023A

Milstar F3, the first Milstar 2, was the first to carry an MDR (medium data rate) payload as well as the LDR. EHF, SHF and UHF coverage. Mass is 4500 kg. Size is 15.5m long 35m span.

Titan 4 B-32 took off from pad 40 at the Cape on 1999 Apr 30, launched by 45SW/3SLS. The vehicle had a 76' fairing. An incorrect constant in the flight software, the roll rate filter constant, was set to -0.199 instead of -1.99, causing extra rolls during the first Centaur burn, depleting the RCS fuel for later burns. SOC-42 control deployed the solar arrays and payload truss wings.

Date	Time	Event	Orbit

Milstar F3



1999 Apr 30	1630	Launch by Titan 4 B-32/TC-14	CC LC40
		T+2:10 Stage 1 burn
		T+2:25 SRMU sep
		T+3:33 Fairing sep
		T+5:25 Stage 2 burn
		T+5:25 Stage 1 sep
		T+9:06 Stage 2 MECO
		T+9:15 Stage 2 sep
	1639	T+9:36s Centaur TC-14 MES-1
	1641	T+11:39s MECO-1	150 x 707? x 28.3
	1735?	T+1:05:01? MES-2
	1740?	T+? MECO-2
	1900?	Centaur TC-14 sep	148.8 700 x 5169 x 28.2
1999 May 6		Orbit raise burns begin
1999 May 10		Orbit raise burns end	153.5 1091 x 5162 x 28.2
1999 May 12		end of ops
Planned
		T+1:05:42 MES-2
		T+1:10:54 MECO-2
		T+6:22:30 MES-3
		T+6:24:41 MECO-3
		T+6:34:54 Centaur sep

Payload:

-X wing
- MDR payload, 32 channels
- Crosslink antenna
- Thrusters
- MDR nulling antennas, 2
- MDR DUC distribution user coverage antennas, 3
+X wing
- Crosslink antenna
- Thrusters
- LDR payload (low data rate), 192 channels
- EHF uplink 44 GHz
- SHF downlink 20 GHz
- SHF Agile beam antennae
- EHF agile antennae
- EHF Earth Coverage
- NSB1 narrow spot beam
- NSB2 narrow spot beam
- WSB wide spot beam
- AFSATCOM IIR payload (UHF, 4 channels)
- Fleet Broadcast channel, UHF
- UHF transmitters (2)

Sports People in the News, 1996

https://welib.org/md5/71596a9c64182adc6358bd74218c980a

Wednesday, May 26, 1999

STS-67 (Endeavour)

1995-007A

Endeavour was launched on Mar 3 into a 346 x 358 km x 28.5 deg orbit to begin the Astro-2 mission. Bad weather at KSC delayed deorbit by one day; in the end Edwards was selected. Mass at deorbit was 104668 kg. Endeavour touched down at Edwards on Mar 18 after a record-breaking flight of 16 days, 15 hours, 8 minutes and 47 seconds.

STS-67 mission events
Date	Time	Event	Orbit
1995 Feb 3	0715	Roll to VAB
1995 Feb 8	1244	Roll to pad 39A
1995 Mar 2	0638:13	Launch
	0640:19	SRB sep
	0646:40	MECO
	0647:00	ET sep	88.64 56 x 358 x 28.5 (OMS dV)
	0718:34	OMS 2 2:58 85m/s	91.59 346 x 358 x 28.47
	0816	PLBD open
	1245	Begin Astro-2 observations
1995 Mar 3			91.59 345 x 359 x 28.5
1995 Mar 9			91.56 342 x 359 x 28.5
1995 Mar 17	0505	End Astro-2 observations
	0536	Stow IPS
	0700		91.54 338 x 361 x 28.5
	1045	Landing waved off
1995 Mar 18	1807	PLBD closed	91.54 336 x 363 x 28.5
	2039:13	OMS deorbit (4:59) 159m/s	88.44 38x 356 x 29.3
	2110:49	Entry interface
	2147:00	Landing EAFB RW22
	2147:15	NGTD
	2147:16	Chute deploy
	2147:45	Chute sep
	2148:00	Wheels stop
1995 Mar 26	1240	SCA	Edwards
	1500	SCA	Dyess AFB, TX
	1930	SCA	Columbus AFB, MS
1995 Mar 27	2247	SCA arrival	KSC SLF
1995 Mar 28	1402	Arrival OPF/1

TDF-2

1990-063A

The second TdF (Telediffusion de France) broadcasting satellite was launched in 1990 Jul. It broadcast 5 French TV channels and two radio stations. In Jul 1997 France Telecom transferred the satellite to Eutelsat. It was moved to 36E for Russian and Central Asian coverage. The satellite is controlled by CNES/Toulouse. Like TDF 1, it suffered transponder failures.

Date	Time	Event	Orbit

TDF 2



1990 Jul 24	2225:00	Launch by Ariane V37	CSG ELA2
		T+2:32 PAL sep
		T+3:36 St 1 sep
		T+3:39 St 2 burn
		T+4:28 Fairing
		T+5:47 St 2 sep
	2230:51	T+5:51 St 3 MES
	2242:51	T+17:51 St 3 MECO
	2245:36	T+20:36 TDF 2 sep
	2247:39	T+22:39 SPELDA sep
	2249:32	T+24:32 DFS 2 sep
1990 Jul 24			705.23 587x39146x62.9
1990 Jul 26			891.03 12749 x 35840 x 1.4
1990 Jul 31?	0900?	LAM?
1990 Aug 6			1436.26 35781 x 35798 x 0.1 GEO 18.7W+0.05W
1990 Aug 7			1436.19 35779x35797x0.06 GEO 18.8W-0.03/d
1990 Aug 22			1436.11 35785x35788x0.04 GEO 18.8W-0.01/d
1990 Sep 10			1436.10 35785 x 35787 x 0.1 GEO 18.8W
1990 Oct		2 transponders failed	1436.10 35782 x 35785 x 0.1 GEO 18.7W
1991 Dec 16			1436.10 35775 x 35797 x 0.0 GEO 18.7W
1993 Aug 16			1436.12 35771 x 35802 x 0.1 GEO 18.9W
1996 May 1			1436.12 35769 x 35804 x 0.0 GEO 18.8W
1997 Jul 6			1436.10 35774 x 35798 x 0.1 GEO 18.8W
1997 Jul 29		Move out?	GEO 19W
1997 Aug		Begin Eutelsat ops
1997 Oct 4			1433.72 35724 x 35755 x 0.1 GEO 26.0E+0.5/d
1997 Nov 18			1436.03 35768 x 35802 x 0.0 GEO 35.6E
1998 Apr 27			1436.04 35758 x 35813 x 0.0 GEO 35.8E
1998 Oct 12			1436.01 35730 x 35839 x 0.0 GEO 36.1E

Aviation Week: January 4,1999

https://welib.org/md5/19f0d79b893c936ce8761ba25266f373

Monday, May 24, 1999

Globalstar 23

1999-004A

Launch 1999 Feb by Starsem Soyuz-Ikar. Ikar flew over 30 missions as a spacecraft propulsion system. Used as Kometa propulsion. The dispenser was built by Aerospatiale/Aquitaine.

Ikar dry mass 820 kg, fuel 842 kg, dispenser 390 kg, satellites dry 1524 kg, fuel for satellites 288 kg, total 3864 kg. Ikar uses 17D61 N2O4/UDMH with 2943 N thrust (3383N including 4 side thrusters) Isp for Ikar is 326 s so Ve = 3197 m/s, mdot = 0.92 kg/s or 1.06 kg/s. (If all fuel used in 610s, mdot is 1.38 kg/s for T=4412N)

Burn 1 was 352s, so 372 kg, dV = ln 3864 / 3492 = 324 m/s. Actual more like 180m/s implies 211 kg used, for mdot of 0.6 kg/s and mean thrust 1.9 kN. This means Ikar mass now 820 + 390 + 631 = 1841 kg. Maybe inefficiencies used up more prop. Ikar is then 820 + 390 + 470 = 1680 kg.

Date	Time	Event	Orbit

Globalstar FM36



1999 Feb 9	0354:00	Launch by Soyuz-U	KB
	0355:58	T+1:58 Blok B-D sep
	0356:38	T+2:38 Fairing sep
	0358:47	T+4:43 Blok A sep, 215 km
	0358:56	T+4:56 Interstage sep
	0402:45	T+8:45 MECO
	0402:48	T+8:48 Stage 3 sep	236 x 884 x 52.0
	0623:31	T+2:29:31 Ikar burn
	0629:23	Ikar MECO after 5:52
	0724:30	T+3:30:30 Sep from Ikar	915 x 947 x 52.0
	0724:34	T+3:30:34 Sep KA-4
1999 Feb 10	0546:48	Ikar deorbit burn 4:18
	0633?	Entry, Impact Pacific 50 55S 140 W
1999 Feb 13			103.59 908 x 947 x 52.0
1999 Feb 25			105.53 1004 x 1033 x 52.0
1999 Mar 4			110.63 1240 x 1270 x 52.0
1999 Mar 8			112.61 1336 x 1355 x 52.0
1999 Mar 14			114.07 1410 x 1415 x 52.0

Tuesday, May 18, 1999

Apollo 10 (Charlie Brown)

1969-043A

Apollo CSM 106, the Apollo 10 CSM, was nicknamed `Charlie Brown' after a comic strip character.

Date	Time	Event	Orbit

CSM 106 Charlie Brown



1969 May 18	1649:00	Launch by Saturn V (SA-505)	KSC LC39B
	1651:15	CECO
	1651:41	OECO
	1651:43	S-IC sep, S-II ignition	-6005 x 112 x 26.9
	1652	T+3:17 LES sep
	1658:12	S-II sep	-2148 x 189 x 32.7
	1658:13	S-IVB MES
	1700:43	S-IVB shutdown
	1700:53	Earth orbital insertion	88.20 185 x 185 x 32.56
	1922:25	TLI burn (5:43)
	1928:10	S-IVB shutdown
	1928:20	Translunar injection	221 x 606571 x 31.74
			220 x 596286 x 31.70 (S4B FER)
	1951:42	T+3:02:42 Sep from S-IVB-505	227 x 607532 x 31.8
	1952:48	T+3:03:48 Sep burn 6.2s 29m/s
	2006:37	T+3:17:37 Docked with LM Snoopy/S-IVB
	2045:26	T+3:56:26 CSM/LM sep from S-IVB
	2128:09	T+4:39:10 SPS sep burn (0:02)
1969 May 19	1921:56	MCC-2
	1922:33	MCC-2 cutoff	-297 x 572699 x 32.0
1969 May 21	0639:50	Equigravisphere
	2045:53	LOI 1 burn (5:56)	109 x -11973 x 155.6 (MR)
	2051:49	LOI	111 x 316 x 174.4
			108 x 311 x 167.8 (MR)
1969 May 22	0114:07	LOI-2 burn	111 x 321 x 174.7 (MR)
	0114:26	LOI-2 cutoff	109 x 113 x 175 (MR)
	1540	CDR and LMP transfer to LM 4
	1900:57	LM 4 undocked	106 x 120 x 173.7
	1936:16	RCS sep burn	107 x 114
	1937:26	RCS burn end
1969 May 23	0311	LM 4 AS docked
	0320?	CDR and LMP return to CSM
	0513:36	LM 4 jettison
	0532:23	RCS sep burn	102 x 117
	0900		104 x 121
1969 May 23		Mass 16670 kg
	2234	Visual on LM DS
1969 May 24	1025:28	TEI burn	93 x 124 x 163.6
	1028:12	TEI	101 x -8080 x 166.7
1969 May 26	1338:57	MCC 7	32 x 3502155 x 29.4
	1339:03	MCC 7 CO	36 x 3525628 x 29.4
	1623:30	SM-106 sep
	1637:54	Entry 11.07km/s	37 x 5929357 x 29.4
			34 x 4120863 x 29.34
	1652:23	Splashdown 15.01S 164.41W POR
	1730	Recovered by USS Princeton

Foton 4

1991-070A

The Foton No. 7 mission was largely commercial, with the Kashtan being used for ESA experiments, and the German COSIMA and French SIDEX supplementary experiments carried as well.

Date	Time	Event	Orbit

Foton No. 7



1991 Oct 4	1810:00	Launch by Soyuz-U	PL LC43/4
	1814	Blok-I burn
	1819	Blok-I sep
1991 Oct 5	1030		90.62 214 x 394 x 62.81
1991 Oct 6	1700		90.59 214 x 392 x 62.80
1991 Oct 7	0700		90.58 214 x 391 x 62.80
1991 Oct 9			90.52 213 x 387 x 62.81
1991 Oct 17	0200		90.35 210 x 373 x 62.81
1991 Oct 18			90.33 210 x 371 x 62.8
1991 Oct 20
	0735?	Deorbit
	0747?	PO sep
	0754?	Entry
	0809?	Landed

Friday, May 14, 1999

Transit O-20

1973-081A

NNS O-20, built by RCA, was launched in Oct 1973, becoming NNS 30200-16.

Date	Time	Event	Orbit

NNS O-20



1973 Oct 30	0037:02	Launch by Scout A S178C	V SLC5
	0038:15	Algol cutoff T+1:13
	0038:15	Castor burn T+1:13
	0038:53	Castor burnout T+1:51
	0039:01	Antares burn T+1:59
	0039:35	Antares burnout T+2:33
	0039:41	Coast
	0049:36	Altair burn T+12:34
	0049:59	Altair cutoff T+12:57
	0055?	X-258 Altair sep
	0055?	Despin weights sep
			105.6 895 x 1149 x 90.2
1995 Jan 31	0434	removed from service

Thursday, May 6, 1999

Kosmos 1401

1982-081A

Resurs F-1 17F41 No. 19 (Kosmos-1401) was launched in Aug 1982.

Date	Time	Event	Orbit

Kosmos-1401



1982 Aug 20	0950	Launch by Soyuz-U	PL LC41
	0958	Blok-I sep
			89.34 216 x 265 x 82.3
1982 Aug 21		Orbit raise	89.90 269 x 274 x 82.3
1982 Aug 29			89.85 260 x 271 x 82.3
1982 Aug 30			90.04 262 x 288 x 82.3
1982 Sep 3			90.01 262 x 285 x 82.3
	0603?	Deorbit
	0612?	PO sep
	0623?	Entry
	0639?	Landed

Monday, May 3, 1999

Kosmos 1218

1980-086A

Date	Time	Event	Orbit

Kosmos-1218



1980 Oct 30	1000	Launch by Soyuz	Baikonur
	1008	Blok I sep
1980 Oct 30			89.73 171x353x64.9
1980 Nov 6			89.70 171x350x64.9 from 89.07 160x299
1980 Nov 10			89.76 171x354x64.9 from 89.22 161x313x64.9
1980 Nov 13		SpK-1 fid
1980 Nov 17			89.60 166x345x64.9 from 89.21 163x308
1980 Nov 21			89.77 199x329x64.9 from 89.17 158x310
1980 Nov 21			89.08 162x297x64.9
1980 Nov 22			89.74 169x355x64.9 from 88.97 161x287
1980 Nov 26		SpK-2 fid
1980 Nov 28			89.67 160x357x64.9 from 89.04 161x294
1980 Dec 3			89.73 172x352x64.9 from 88.96 152x296
1980 Dec 12			88.73 156x268x64.9
1980 Dec 15
	2019?	Deorbit
	2033?	Entry
	2045?	Land

Kosmos 1122

1979-075A

The last Zenit-2M/NKh mission carried a 31KS Nauka capsule.

Date	Time	Event	Orbit

Kosmos-1122



1979 Aug 17	0745	Launch by Soyuz	PL
	0749	Blok-I burn
	0753	Blok-I sep
1979 Aug 17			89.01 212x234x81.32
1979 Aug 17			89.06 214x239x81.34
1979 Aug 30			88.73 199x222x81.35
1979 Aug 30
	0338?	Deorbit
	0347?	PO sep
	0354?	Entry	-209 x 197 x 81.35
	0412?	Landed

Saturday, May 1, 1999

Kosmos 1606

1984-111A

Date	Time	Event	Orbit

Kosmos-1606



1984 Oct 18	1746	Launch by 11K68	Plesetsk
		T+2:00 St 1 sep
		T+3:33? GO sep
		T+4:38? St 2 sep
		T+5:20? S5M burn 1
	1751	T+6:48 S5M MECO1 km	60? x 650 x 82.5
		T+40:58? S5M burn 2
		T+41:08? S5M MECO2
	1827?	T+41:38? S5M sep
1984 Oct 18			632x678x82.5

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