The Polar Satellite Launch Vehicle, or the PSLV to you and me, is an interesting piece of machinery. It's significance, utility and the tremendous service that it has rendered so far to the Indian space programme has been taken for granted, purely due to its near-impeccable record. So much so that a failed launch of a PSLV would garner more attention than its past successes, but then that, I believe is the way our heroes are always treated.
With the journey of Mangalyaan close to being initiated (the slated date of launch being October 28, 2013) and the PSLV yet again acting as the ferrying service to the hitch-hiking orbiter, it would pay to glance over the life and times of the highly functional and widely respected PSLV...
A slingshot into space
The PSLV is basically an expendable launch vehicle (ELV), which means that it is operated on a use-and-throw basis in each launch. Typically it consists of more than one component, aka stages, which drop off one by one to the earth after being launched, except the last stage, which catapults the hitch-hiker, aka the payload, into its orbit around the earth. The other kind is the Reusable Launch Vehicle (RLV), almost of the kind that NASA used to maintain till 2011 in the form of its Space Shuttle fleet (comprising of four orbiters Enterprise, Columbus, Challenger, Discovery and Atlantis). These Shuttles consisted of three components - the orbiter vehicle (OV) which carried the payload, the external tank (ET) and the solid rocket boosters (SRB)- of which two, viz. the OV and the SRB return to the good earth, and after some polishing-up, could be reused for subsequent flights.
So what is this ride made of ?
Plenty of parts, it seems; the most basic components being the several stages of rockets and a set of SRB. Now let us remember that a rocket is just a vehicle, with a potent mixture of fuel/propellants splashing inside it, which when ignited, belch a massive exhaust backwards/downwards. The exhaust, in full deference to Newton's Third Law of Motion, pitches the vehicle forward/upward. This is the guiding principal of each of the four rocket stages used in the PSLV.
Speaking of propellants, they are of five kinds: Solid, liquid, gaseous, hybrid and gels. The PSLV use only the solid and liquid kind, so we shall temporarily forget about the other three varieties. Both solid and liquid propellants are basically one big mixture of oxidising (one that yields oxygen) agents and reducing agents (the fuel which starts crackling when it meets the oxygen), the difference being only in their respective states of existence. The underlying principle is that of the good old combustion: the oxidising agent meets the reducing agent, and a merry bonfire erupts, only a few thousand times stronger than the one in your backyard.
So every PSLV comprises of four stages: PS1 to PS4. A brief summarisation of each stage is as given below:
SOM (or PSOM) stands for Strap-on Motors,which is another way of addressing the SRB. The PSLV is armed with 6 PSOM, four of which are fired on the ground and two are air lit.
The PSLV has completed 22 successful flights, in addition to the first ever launch of the PSLV D1 which filed 700 seconds into its flight, while another launch was at best only a partial failure as in the satellite was launched, albeit at a different orbit than previously decided. As the table indicates, ISRO currently uses three variants of the PSLV: the Regular (which is just called the PSLV), the Core-Alone (CA) configuration and the PSLV-XL. The initial launches of ISRO have all been made through the Regular PSLV, which has been comprises all the four rocket stages and the additional PSOM.
The typical PSLV stands nearly 44 meters tall, and has a liftoff mass of 295 tonnes, with a capability to carry payloads of about 1678 kilogrammes to a 622 kilometres sun-synchronous orbit (viz. this orbit has a particular altitude and inclination to it, so that the satellite passes over the same point on the earth at approximately the same local time daily.
The CA configuration, as the name suggests, is the bare rocket stages, with no add-ons. It weighs around 230 tonnes and is currently designed to catapult a 1100 kilogramme payload into a 622 kilometres sun-synchronous orbit.
What we should actually focus on, is the PSLV-XL. The first time this juggernaut of a vehicle was used (in the form of PSLV C-11) happened to be that historic day of October 22, 2008, when the Chandrayaan - I was launched towards our only natural satellite. This brute is 44.4 metres tall and has a lift-off mass of 320 tonnes. Though the first stage, which was taller by 0.20 metres for C11, holds the same mass of propellants as the other variants, each of the six,extended and more powerful PSOM carry 12 tonnes of the solid propellant (as compared to only 9 tonnes in the other variants), capable of producing a maximum thrust of 720 kilonewtons. The fourth stage of the launch vehicle with a twin-engine model, is powered by 2.5 tonnes of liquid propellant. The PSLV-XL is capable of launching payloads as heavy as 1800 kilogrammes. The C11 had launched the 1380 kilogramme moon orbiter and impactor in the 2008. Chandrayaan mission. Subsequent PSLV-XL have been used to launch progressively heavier payloads upto 1850 kilogrammes.
Needless to say, there are sceptics all over the place, writing off this mission even before it has begun, but Mangalyaan, if successful, would be a tremendous boost to the Indian Space Programme. More than anything else, it would be a nod to the strides that are being taken in the field of science, which frankly, hasn't been quite something to boast about. It is no doubt going to be a momentous step for ISRO, and one of the numerous components this mission depends on is this particular vehicle, which has had quite an enviable reputation. The 'wokhorse' of ISRO is still, proudly, in service.
So every PSLV comprises of four stages: PS1 to PS4. A brief summarisation of each stage is as given below:
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| Source: www.isro.org Figures indicate values averaged over the respective number of successful launches, based on publicly available information with ISRO |
SOM (or PSOM) stands for Strap-on Motors,which is another way of addressing the SRB. The PSLV is armed with 6 PSOM, four of which are fired on the ground and two are air lit.
The PSLV has completed 22 successful flights, in addition to the first ever launch of the PSLV D1 which filed 700 seconds into its flight, while another launch was at best only a partial failure as in the satellite was launched, albeit at a different orbit than previously decided. As the table indicates, ISRO currently uses three variants of the PSLV: the Regular (which is just called the PSLV), the Core-Alone (CA) configuration and the PSLV-XL. The initial launches of ISRO have all been made through the Regular PSLV, which has been comprises all the four rocket stages and the additional PSOM.
The typical PSLV stands nearly 44 meters tall, and has a liftoff mass of 295 tonnes, with a capability to carry payloads of about 1678 kilogrammes to a 622 kilometres sun-synchronous orbit (viz. this orbit has a particular altitude and inclination to it, so that the satellite passes over the same point on the earth at approximately the same local time daily.
The CA configuration, as the name suggests, is the bare rocket stages, with no add-ons. It weighs around 230 tonnes and is currently designed to catapult a 1100 kilogramme payload into a 622 kilometres sun-synchronous orbit.
What we should actually focus on, is the PSLV-XL. The first time this juggernaut of a vehicle was used (in the form of PSLV C-11) happened to be that historic day of October 22, 2008, when the Chandrayaan - I was launched towards our only natural satellite. This brute is 44.4 metres tall and has a lift-off mass of 320 tonnes. Though the first stage, which was taller by 0.20 metres for C11, holds the same mass of propellants as the other variants, each of the six,extended and more powerful PSOM carry 12 tonnes of the solid propellant (as compared to only 9 tonnes in the other variants), capable of producing a maximum thrust of 720 kilonewtons. The fourth stage of the launch vehicle with a twin-engine model, is powered by 2.5 tonnes of liquid propellant. The PSLV-XL is capable of launching payloads as heavy as 1800 kilogrammes. The C11 had launched the 1380 kilogramme moon orbiter and impactor in the 2008. Chandrayaan mission. Subsequent PSLV-XL have been used to launch progressively heavier payloads upto 1850 kilogrammes.
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| The PSLV C-11 at the Vehicle Assembly Building Image: Courtesy ISRO |
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| PSLV C-11 liftoff Image: Courtesy ISRO |
Needless to say, there are sceptics all over the place, writing off this mission even before it has begun, but Mangalyaan, if successful, would be a tremendous boost to the Indian Space Programme. More than anything else, it would be a nod to the strides that are being taken in the field of science, which frankly, hasn't been quite something to boast about. It is no doubt going to be a momentous step for ISRO, and one of the numerous components this mission depends on is this particular vehicle, which has had quite an enviable reputation. The 'wokhorse' of ISRO is still, proudly, in service.
Sources: www.isro.org/www.spaceflight101.com/www.nasa.gov
Images courtesy ISRO








