Which fuel is used in GSLV?
Second Stage: GS2
| Engine | : Vikas |
|---|---|
| Fuel | : UDMH + N2O4 |
| Max. Thrust | : 800 kN |
| Burntime | : 150 sec |
Which fuel is used in SLV?
It was a four-stage rocket with all solid-propellant motors. The first launch of the SLV took place in Sriharikota on 10 August 1979….Satellite Launch Vehicle.
| Size | |
|---|---|
| Propellant | PBAN (Polybutadiene acrylonitrile) Solid |
| Second stage | |
| Propellant mass | 3 tonnes |
| Powered by | 1 solid |
Is GSLV made in India?
Geosynchronous Satellite Launch Vehicle (GSLV) is an expendable launch system operated by the Indian Space Research Organisation (ISRO)….Geosynchronous Satellite Launch Vehicle.
| GSLV-F05 carrying INSAT-3DR at the Second Launch Pad | |
| Has use | Medium Lift Launch System |
| Manufacturer | ISRO |
| Country of origin | India |
| Size |
|---|
Who makes rocket engines for ISRO?
Vikas (rocket engine)
| Model of the Vikas engine | |
| Country of origin | India |
| Designer | ISRO |
| Manufacturer | Godrej & Boyce and MTAR Technologies |
| Liquid-fuel engine |
|---|
Which is better PSLV or GSLV?
Difference between PSLV and GSLV GSLV has the capability to put a heavier payload in the orbit than the Polar Satellite Launch Vehicle (PSLV). PSLV can carry satellites up to a total weight of 2000 kg into space and reach up to an altitude of 600-900 km. GSLV can carry weight up to 5,000 kg and reach up to 36,000 km.
Which solid fuel is used in PSLV?
It uses the S139 solid rocket booster that contains 138 tonnes of HTPB. While the PSLV-G uses 6 HTPB based solid strap-on motors of 9 tonnes each and PSLV-XL uses 6 extended strap-ons of 12 tonnes each, the PSLV-CA (core alone version) does not use any strap-on motors.
What is GSLV for?
Definition: Geosynchronous Satellite Launch Vehicle (GSLV) is a space launch vehicle designed, developed, and operated by the Indian Space Research Organization (ISRO) to launch satellites and other space objects into Geosynchronous Transfer Orbits.
What are the 3 stages of GSLV?
GSLV MkIII is configured as a three stage vehicle with two solid strap-on motors (S200), one liquid core stage (L110) and a high thrust cryogenic upper stage (C25).
Is Vikas engine a Cryogenic?
The Indian Space & Research Organisation (Isro) successfully test-fired the Vikas engine that will power the ambitious Gaganyaan mission into space. The high thrust test came nearly a week after the agency conducted the qualification test of the Cryogenic Engine by firing it for a duration of 720 seconds.
What is the meaning of GSLV d6?
GSLV-D6 is the ninth flight of India’s Geosynchronous Satellite Launch Vehicle (GSLV). It is also the fifth developmental flight of GSLV and third time the indigenously developed Cryogenic Upper Stage (CUS) is being carried on-board during a GSLV flight.
Which engine is used in the second stage of GSLV?
One Vikas engine is used in the second stage of GSLV. The stage was derived from the PS2 of PSLV where the Vikas engine has proved its reliability. Max. Thrust The first stage of GSLV was also derived from the PSLV’s PS1. The 138 tonne solid rocket motor is augmented by 4 liquid strap-ons. Max. Thrust
What are the payloads of GSLV?
GSLV’s primary payloads are INSAT class of communication satellites that operate from Geostationary orbits and hence are placed in Geosynchronous Transfer Orbits by GSLV. Further, GSLV’s capability of placing up to 5 tonnes in Low Earth Orbits broadens the scope of payloads from heavy satellites to multiple smaller satellites.
What is cryogenic upper stage of GSLV Mk II?
The indigenously developed cryogenic Upper Stage (CUS), which is flight proven, forms the third stage of GSLV Mk II. From January 2014, the vehicle has achieved four consecutive successes. At a diameter of 3.4 m, the payload fairing of GSLV is wider than the rest of the launcher.