Truth or Dare

https://welib.org/md5/246f27bcd26ebb81e17f1b001edb747e

Moon lander : how we developed the Apollo lunar module

 https://welib.org/md5/60abb9a85d64fe2c8e5bc7eef03d700e

Aviation Week: September 8,2003

 https://welib.org/md5/0ccdc62f7a44e16042437b0f7da34dd7

Intelsat 502

 1980-098A

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The first Intelsat 5 was flight vehicle 2, launched late on 1980 Dec 6.

Intelsat V F-2
Date	Time	Event	Orbit
1980 Dec 6	2331:01	Launch by Atlas Centaur	CC LC36
		T+2:23 Booster sep
	2334	T+3:33 Fairing sep
		T+4:15 SECO
	2335	T+4:17 Atlas sep
	2335	T+4:23 MES-1 5:12
	2340	T+9:35 MECO-1	89.57 148 x 358 x 28.31
	2356	T+25m MES-2 1:24
	2357	T+26m MECO-2 Centaur MECO	630.13 226 x 35711 x 23.7
1980 Dec 6	2358	T+27:31 Centaur sep
1980 Dec 7	0001	T+30:31 Centaur venting
	0600?	Apo 1 over 90E
	1600?	Apo 2 over 60W
1980 Dec 8	0300?	Apo 3 over 135E
	1300?	Apo 4 over 15W
1980 Dec 8	1232	Star 37F burn 42s? (or 62s?) 1.83km/s	1417.56 35141 x 35704 x 0.9
1980 Dec 9			1432.19 35666 x 35754 x 0.9 GEO 14.5W+1.0E
1980 Dec 9	0930?	Orbit adjust
1980 Dec 10	1200	Spindown, sun acquisition
		3-axis, antennae and solar panels deployed
1980 Dec 10			1431.02 35639x 35735 x 0.9 GEO 11.6W+1.2E
1980 Dec 10			GEO +1/d
1980 Dec 19			1430.97 35638 x 35733 x 0.8 GEO 0W+1.3E
1981 Jan		Tests from Fucino	GEO 15E
1981 Mar 17			1436.13 35764 x 35809 x 0.7 GEO 20.1W
1981 Mar 17		mv in, probs. with sensors	GEO 20W
1981 May		Locate for spacing with F1	GEO 18.1W
1981 May 26			1436.18 35763 x 35812 x 0.5 GEO 18.3W
1981 Jun 11			GEO 18.6W +0.03E/d
1981 Jun 28			1436.23 35762 x 35816 x 0.5 GEO 19.2W
1981 Jul 29			1436.11 35771 x 35802 x 0.4 GEO 21.6W
1981 Aug 1		Op. spare	GEO 22W
1981 Oct 21			1436.11 35775 x 35797 x 0.3 GEO 21.5W
1981 Oct 29		mv out
1981 Nov 2			1436.81 35781 x 35819 x 0.2 GEO 23.5E+0.2W
1981 Dec 2		mv in	1436.38 35778 x 35805 x 0.2 GEO 27.8W+0.08W
1981 Dec 16			1436.15 35773 x 35802 x 0.1 GEO 27.6W
1982 Nov 9			1436.22 35774 x 35803 x 0.1 GEO 27.7W
1982 Dec		AOR C/DL	GEO 27.4W
1983 Jan 23			1436.10 35767 x 35806 x 0.0 GEO 27.5W
1983 Jan 25		mv out
1983 Feb 6		AOR Major Path 1	1436.02 35775 x 35794 x 0.1 GEO 34.4W
1983 Jun 8			1436.11 35770 x 35803 x 0.1 GEO 34.5W
1985 Mar			GEO 34.5W
1985 May 21			1436.15 35764 x 35811 x 0.0 GEO 34.6W
1985 May 31		mv to 27W	1436.00 35768 x 35800 x 0.1 GEO 27.5W
1985 Jun 13			1436.09 35773 x 35798 x 0.0 GEO 27.4W
1985 Jun		Move to 1.0W
1985 Jul 16			1436.14 35778 x 35797 x 0.1 GEO 1.0W
1985 Aug			GEO 1W
1986 Sep			GEO 1W
1989 May		Replaced by 512
1989 May 26			14536.06 35769 x 35802 x 0.6 GEO 1.0W
1989 May 27		mv out	1437.35 35801 x 35820 x 0.6 GEO 2W+0.3W
1989 Aug 2		mv in	1436.15 35773 x 35802 x 0.7 GEO 21.5W
1990 Jan		AOR	GEO 21.5W
1991 Dec		AOR	GEO 21.2W
1992 Aug 3			1436.08 35767 x 35805 x 3.5 GEO 21.3W
1994 Oct 11			1436.15 35770 x 35805 x 5.2 GEO 21.4W
1994 Oct 28		mv out	1437.41 35801 x 35823 x 5.2 GEO 32.1W+0.3W
1994 Dec 15		mv in	1436.18 35774 x 35801 x 5.3 GEO 40.4W
1995 Feb 27			1436.04 35771 x 35799 x 5.5 GEO 40.3W
1998 Apr 8			1436.13 35772 x 35802 x 7.5 GEO 40.5W
1998 Apr 14		orbit raise	1448.73 35988 x 36079 x 7.5
1998 Apr 17		orbit raise	1456.26 36099 x 36261 x 7.5
1999 Apr 26			1456.25 36119 x 36240 x 8.0

IDCSP 2

  1967-003A

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The second IDCSP launch left the pad on 1967 Jan 18 carrying satellites 9321 to 9328 (IDCSP 8 to 15), a total payload of 467 kg. The first satellite of the batch, IDCSP 8, was deployed into a 1329.6 min orbit.

IDCSP 8
Date	Time	Event	Orbit
1967 Jan 18	1419	Launch by Titan IIIC (3C-13)	CK LC41
		T+1:50 Core MES
		T+2:03 Solids sep; 45 km?
		T+3:30 Fairing 130 km
		T+4:29 St 1 sep
		T+4:29 St 2 MES
	1426	T+7:43 St 2 MECO	-500? x 160 x 28.6
		T+7:53 St 2 sep
		T+7:56? Transtage MES
	1431	T+12:12? Transtage MECO-1	171 x 182 x 28.6
	1537?	Transtage MES-2
	1538?	Transtage MECO-2	193 x 33810 x 26.4
	2027?	Transtage MES-3
	2028?	Transtage MECO-3
	2030	T+6:11 IDCSP 8-15 separate
			1329.6 35557 x 33800 x 0.07