Progress M-52

 2005-007A

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Spacecraft 11F615A55 No. 352 on mission 17P. Included the PCE (Proximity Communications Equipment) to be installed on ISS for the ESA ATV.

Mass 7259 kg launch, 6966 kg docking.

 

Progress M-52
Date	Time	Event	Orbit
2005 Feb 28	1909:18	Launch by Soyuz-U No. 093	KB LC1/5
		T+1:59 Strapon sep
		T+2:41 GO sep
		T+4:47 Blok A Sep
		T+4:57 KhO sep
	1918:03	T+8:45 MECO
	1918:07	T+8:49 sep
2005 Mar 1	0051	DV1 17m/s
	0137	DV2 8m/s
	1954	DV3
2005 Mar 2	1817:33	DV 24 m/s
	1842:45	DV 1 m/s
	1903:31	DV 25 m/s
	1945	DV 8.8m/s
	1950	Begin flyaround
	1951:42	5 m/s, at 1 km
	1954	2m/s, 550 m
	1959	Stationkeep at 160m
	2002	Resume approach
	2010:08	Docked with Zvezda
	2019:10	DV 0.7m/s 15s
2005 Jun 15	2016:10	Undock
	2316:00	Deorbit 85.8m/s 162.1s	347 x 353 x 51.6
	2319:12	DO CO	56 x 353 x 51.6
	2351:27	Entry

Cosmos 1

 2005-F02

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Orbital launch Volna late 2001. Built by NPOL/Babakin. 850 x 850 km orbit. 8 blades, 600 m2 aluminized mylar.

Mass 103 kg on orbit (23 kg sail) with 8 15-m petals, spanning 30m. Petals are 5 micron aluminized Mylar polyethlteraphtalate, inflated with nitrogen. Expected solar thrust is 5mN.

Has nosecone: blunt cone 1.1d 1.75l TPS Apogee motor 0.42d 0.50?l Isaev liquid engine UDMH/N2O4, 240s burn giving 0.9?km/s.

S/C 1.1l 1.1d cone-cylinder-cone (two cones connected by small cylinder); deployed 28.8d with 8 blades.

Control from Babakin/Moskva.

Cosmos sail
Date	Time	Event	Orbit
2005 Jun 21	1946:09	Volna launch from Borisoglebsk
		Stage 1 sep
		Stage 2 sep
		Stage 3 burn
	1952:27	T+6:18 Stage 3 sep	-2000? x 765 x 80
		T+15 min telemetry starts
	2005:22	T+19:13 Apogee engine burn
		AKM sep	832 x 840 x 78.6
		Plume shield sep (planned)
		Spinup to 95 rpm (planned)
		Solar sail deploy(planned)
	2007	T+21 min loss of telemetry
		Spindown
	2019?	Reentry?

Payload:

• 8-bladed solar sail

• UHF, S-band radio systems

• Advanced Pixel Sensor CMOS camera

• CCD rotating Matrix camera (Mars-96 model)

• Microaccelerometers

• Charged particle environment monitor