GSLV Mk.3

GSLV Mk.3 [ISRO]

GSLV Mk III is envisaged to launch four tonne satellite into geosynchronous transfer orbit. GSLV-Mk III is a three-stage vehicle with a 110 ton core liquid propellant stage (L-110) and a strap-on stage with two solid propellant motors, each with 200 tons propellant (S-200). The upper stage will be cryogenic fueled with a propellant loading of 25 tons (C-25). GSLV Mk-III will have a lift-off weight of about 629 tons and will be 42.4 m tall. The payload fairing will have a diameter of 5 m and a payload volume of 100 cubic meters.

Version	Strap-On	Stage 1	Stage 2
GSLV Mk.3 (1 st.)	2 S-200	L-110 / 2 Vikas	Dummy C-25
GSLV Mk.3	2 S-200	L-110 / 2 Vikas	C-25 / CS

Performance (kg)	LEO	LPEO	SSO	GTO	GEO	MolO	IP
GSLV Mk.3				4000

No: TypeNo:Serial     Type              Date           LS       Payload

none


Planned:
 1       1            GSLV Mk.3 (1st)   xx.xx.2012  *  Sr SLP   (R&D)  
 2       1            GSLV Mk.3         xx.xx.xxxx     Sr       GSat 10   
 3       2            GSLV Mk.3         xx.xx.xxxx     Sr       GSat 11