Block-D, Gallery

Launch vehicle	Spacecraft	Block		Operated 30.03.2012	Engine		Propulsion	Thrust (vac)	Isp (vac)	Fuel mass	Burn time	Flow rate
Launch vehicle	Spacecraft	Block		Operated 30.03.2012	Engine		Propulsion	kN	Nskg	t	s	t/s
N-1 (5th stage)		D		-	Sl-5400		T-1/LOX	82.38	3393	14.57	600	0.0226
Energiya	Buran shuttle	OMS (1)	17D12	-	RD-58S	17D11	Syntin/LOX	86.30	3540	7.24	297	0.0244
Proton 4th stage		D	11S824	40	RD-58	11D58	RG-1/LOX	83.36	3422	11.45	470	0.0244
		D-1	11S824M	12				83.36	3452	12.56	520	0.0242
	Phobos, Mars 8	D-2	11S824F	3				83.36	3452	14.97	620	0.0242
		DM	11S86	66	RD-58M	11D58M		83.61	3462	15.22	630	0.0242
	Inmarsat	Dm1		1
		DM-2	11S861	113						15.46	640
	Oko-S	Dm2		6
		DM-2M-01 (DM-2M)	11S861-01	14						15.94	660
		DM-3		24						16.42	680
	Uragan-M	DM-2M-03 (Dm3)	11S861-03	1						18.63	770
	Telstar 5	Dm4		1
	ARAKS	Dm5	17S40	2
Zenit 3SL		DM-SL		31	RD-58Z	11D58Z		79.46	3510	15.85	700	0.0226
Zenit 3SLB		DM-SL		5
Kvant		DM-SL		-
Energiya-M		DM		-	RD-58M	11D58M		83.61	3462	15.71	650	0.0242
Samara		-		-	RD-58M
Aurora-L.SK		DM		-	RD-58M			72.46	3462	12.56	600	0.0209
Yamal (ex Aurora)		Block 2 (Corvet)		-	RD-58MFD			78.42	3668	10.16	475	0.0214
Polyot Air launch		DM		-	RD-58MFD			78.42	3668	14.97	700	0.0214

Note: The Block DM-2M-03 (=Dm3, 11S861-03) upper stage was developed primarily to increase the performance of Zenit-3SL rockets.
The maiden flight of the Block Dm3 failed on Dec. 05, 2010 during a mission to deliver a trio of GLONASS satellites onboard a Proton-M rocket.
Block Dm3 had approximately 25 percent larger propellant tanks than the previous version of the stage. With 2,000 kilograms of extra propellant, which was believed to be mistakenly loaded onboard, the tanks would be filled close to the same level as the old ones - the oxygen tank would be
90 percent full with a 25-percent reserve load.
Source: RussianSpaceWeb

Engine RD-58M

The failed new Block Dm3

Block DM back side

Block DM front side (Proton-KM)

Proton-KM (Uragan)

Block DM-SL (Zenit 3SL)

Block DM-SL (Zenit 3SLB)