Progress M-11M

 2011-027A

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Flight 43P, spacecraft 11F615A60 No. 411. Mass 7285 kg launch, 6176 kg undocking. Cargo mass 2673 kg.

M11M
Date	Time	Event	Orbit
2011 Jun 21	1438:15	Launch by Soyuz-U	KB LC1
	1442	Blok A sep
	1447	Blok I MECO	188 x 218 x 51.6
	1822:24	DV1 35.8m/s 90s
	1911:26	DV2 21.9m/s 55s
2011 Jun 22	1556:35	DV 19.1s 1.3m/s
2011 Jun 23	1308		288 x 322 x 51.6
	1637	Docked Zvezda aft
2011 Jun 27			92.18 373 x 388 x 51.6
2011 Jun 29	1215	Reboost DPO 33:31
	1248	End reboost 2.2m/s
2011 Jul 1	1216	2.0m/s orbit boost 29:32 301 kg
2011 Aug 23	0934	Undocked Zvezda
	0937:32	Undocked Zvezda / sep?
	0941	Sep burn 15s 0.7m/s
	1246	SKD phasing burn 4.5m/s
2011 Aug 27	1153:34	Radar-4 experiment, burn 1 4.5m/s
2011 Aug 28	1050:10	Burn 2
2011 Aug 29	1121:38	Burn 3
2011 Aug 30	1016:59	Burn 4
2011 Aug 31	1047:41	Burn 5
2011 Sep 1	0934:31	Deorbit 180s 91.8m/s
	1021:41	Entry, 40 08S 135 02 W

The Mercury Seven

 https://content.blubrry.com/spacerockethistory/SRH-2013-06-21-017.mp3

The preppy cookbook : classic recipes for the modern prep

 https://welib.org/md5/b47860edc097fb66c605c42520938702

The New Yorker: February 11-18,2013

 https://welib.org/md5/26e413482cf53573061b860b8fa5081d

Space Enterprise: Living and Working Offworld in the 21st Century

 https://welib.org/md5/ba077e85f79d478e8fc02f43c3b6d579

Odin

 2001-007A

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SSC's Odin astronomy satellite will fly on an STC-Komplex Start-1 in 1998 from Svobodny.

Odin has a dual mission to study the interstellar medium and aeronomy. The astronomy mission involves 500 GHz and 119 GHz observations of molecular clouds and other sources. The aeronomy part studies the stratosphere and mesosphere, scanning the earth limb from 15 to 120 km. It will study the ozone layer.

Mass is 250 kg; size box + plate + antenna 2.0m h 3.8m span 1.1m packed dia. 1800 LT SSO. The spacecraft has four solar manels mounted on the aft sunshade. Odin is built by SSC. SSC reports to SNSB (Swedish National Space Board).

DS stage remained attached to St 4?

The astronomy part of the mission ended in spring 2007. In 2008 Odin's mission was extended again as it continued climate change studies.

Odin
Date	Time	Event	Orbit
2001 Feb 20	0848:27	Launch by Start-1	SVOB
	0849?	T+1m Stage 2 burn
	0850?	T+2m Stage 3 burn
	0854?	T+6m Stage 4 burn
	0854?	T+6m Stage 4 burnout	96.53 576 x 606 x 97.8
		DS burn
		Debris G	531 x 610 x 97.8
		Debris C-F,H,J
	0855?	T+7m DS burn?
	0902?	DS burnout?
	0904:35	Sep from stage 4
	2200		97.03 610 x 621 x 97.8
2007 Mar?		end of astro ops
2013 Jun		Still op for climate change study

Payload:

• 1.1m reflector

• SMR 500 GHz radiometer

• SMR 119 GHz radiometer (O2 ground state)

• OSIRIS Optical/IR spectrometer 2800-8000A, 1.27mu, 3cm aperture

Intelsat 15

 2009-067A

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Launch by Zenit-3SLB wth 2SB60 No.4 and DM-SLB No. 4L.

2484 kg OSC Star-2.4 for Middle East, IOR and Russia.

IS-15
Date	Time	Event	Orbit
2009 Nov 30	2100:01	Launch by Zenit-3SLB No. 4	KB
		T+2:29 St 1 sep
		T+5:16 PLF sep
		T+8:31 Stage 2 sep	-2159 x 359 x 51.35
		Adapter sep	-2134 x 346 x 51.34
	2108	T+8:41 MES-1	-2134 x 346 x 51.34
	2112	T+12:08 MECO-1 371 km	197 x 632 x 51.35
	2220	T+1:20:14 MES-2
	2225	T+1:25:35 MECO-2 340 km	215 x 36071 x 49.0
			200 x 35907 x 48.93 (TLE)
2009 Dec 1
	0314	T+6:14:03 MES-3
	0314?	T+6:14:51? MECO-3
	0326	T+6:26:42 DM sep	10290 x 35786 x 12.0
2009 Dec 3			829.55 9965 x 35768 x 11.9
2009 Dec 3			1059.89 20338 x 35775 x 4.7
2009 Dec 4			1340.14 31990 x 35783 x 0.8
2009 Dec 6	0515?	LAM
2009 Dec 7			1435.17 35754 x 35781 x 0.0
2010 Jan 22			1436.11 35759 x 35814 x 0.0 GEO 85.1E
2010 Apr 29			1436.10 35775 x 35797 x 0.1 GEO 85.1E

May 18,2005

 https://en.wikipedia.org/wiki/Margaret_Thatcher

Rassvet

 2010-019

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MIM-1 (SGM) Maliy Issledovatelskiy Modul-1/Stikovochno-gruzovoi modul (Mini Research Module/Docking and Cargo Module) is built under contract to NASA. Mass 7900 kg, size 6.6m long 2.4m dia.

Rassvet itself is 4780 kg empty plus 1400 kg of US cargo, total 6180 kg. With the external material of 1720 kg the laucnh package is 7900 kg.

Per STS-132 PK, mass is 8015 kg loaded, 5075 kg empty so 2940 kg cargo. PK calls out 1392 kg ISS supplies and 1310 kg EJ/PWP/AL/Rad (so 238 kg missing). But other data gives 1720 kg for EJ/PWP/AL/Rad which would imply 1220 kg ISS supplies.

Launch by STS-132/ULF-4, install at Zarya nadir.

1400 kg US cargo inside, 1800 kg cargo outside.

Rassvet MIM-1 is a modified stretched Soyuz BO?

521GK.

Payload:

• MLM airlock 900 kg

• MLM radiator 570 kg

• ERA spare elbow joint (EJ) 150 kg

• PWP, Portable Work Post, ERA workstation 100 kg