OUTER SPACE (THE KNOWN HIDDEN FACTS)

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10 Recent Space Discoveries No One Can Explain


The universe loves to confuse us. And sometimes, the discoveries that benefit science the most are those that leave us severely confused and scrambling for crazy explanations.

10The Moon’s Mysterious Magnetic Field

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Photo credit: Mark A. Wieczorek
The Moon has remained magnetically inert for eons, but new research confirms that this was not always the case. Over four billion years ago, an inner molten moon-core whirled against a lunar mantle, much like Earth’s own dynamo, and a potent magnetic shield extended from the Moon. But this was presumably a much weaker version than Earth’s, since the satellite obviously lack’s Earth’s heft, right?
Surprisingly, our scrawny little moon was actually able to generate a mightier field than ours. No one knows why such a puny body displayed such potent magnetic activity, with current answers running the gamut from “we don’t know” to “magic?” The mystery reveals that there’s yet another unknown set of variables regarding our most intimately studied partner. It appears the early Moon took advantage of some exotic method to produce its awesome magnetic field. And it managed this for longer than astronomers previously thought was possible, perhaps due to constant meteor impacts that fueled Luna’s magnetism.
It appears that the field disappeared sometime around 3.8–4 billion years ago, though more research is necessary to find out exactly why. Surprisingly, studies suggest that the Moon’s core is still at least slightly liquid. So even though the Moon is within reaching distance, we’re constantly reminded that there are many fundamental questions we’ve yet to answer about lunar geology.

9Galaxies 13 Billion Years Old

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Photo credit: University of Tokyo
The early universe was an approximation of hell—a roiling, opaquely dense stew of electrons and protons. Almost half a billion years passed before the baby universe cooled down enough to allow the formation of neutrons. Shortly thereafter, the universal landscape settled further so that stars and galaxies could come into being.
A recent ultra-deep survey by the Subaru telescope—located in Hawaii and run by the National Astronomical Observatory of Japan—revealed seven of the earliest galaxies ever. Over 13 billion light-years distant, they appeared as unimaginably faint pinpricks of light. In fact, they were visible only after Subaru focused on a tiny patch of sky for over 100 hours of exposure.
Born only 700 million years after the big bang exploded everything into existence, these galaxies are among the earliest things ever observed and are among the first evidence of organization within the universe. These types of galaxies are characterized by intense hydrogen excitation and an absence of heavier elements since metals (other than minute amounts of lithium) hadn’t been blasted into existence yet by supernovae.
Termed Lyman-alpha emitters (LAE), these galaxies appeared suddenly and for (more or less) unknown reasons. LAE galaxies are prolific star-producers, and their extreme age offers insight into the evolution of the universe. However, astronomers aren’t sure if the ones captured by Subaru were newly formed or if they’d been present and were only made visible by a thinning of the cosmic gas that initially obscured them.

8Titan’s Magic Island

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Saturn’s largest moon, Titan, might be the most intriguing member of the solar system. It’s a primeval Earth, complete with an atmosphere, liquid bodies, and even suggestions of geological activity.
In 2013, the orbiting Cassini spacecraft spotted a brand new chunk of land that mysteriously appeared out of Titan’s second-largest sea, Ligeria Mare. Shortly thereafter, the “Magic Island” disappeared just as mysteriously into the translucent, –200 degree Celsius (–290 °F) methane-ethane sea. And then it reappeared again as a much larger landmass during one of Cassini’s recent radar sweeps of Titan.
The transient land confirms the supposition that Titan’s alien oceans and seas are dynamic components of an active environment, rather than static features. However, astronomers are at a loss to explain the physical processes responsible for the ephemeral landmass. Especially since it appears to have doubled in size—from 50 to 100 kilometers (30 to 60 mi) across—since it reappeared.

7The Asteroid With Rings

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All our gas giants are encircled by rings, though most of these are tenuous wisps of debris quite unlike Saturn’s massive sets of bling. And now, for the first time and quite unexpectedly, astronomers have found rings around a much smaller body. Meet Chariklo, an asteroid measuring only 250 kilometers (155 mi) across yet boasting its own ring system.
Chariklo, though the largest object in its cosmic vicinity, looked like an unremarkable chunk of space rock. Then astronomers noticed its anomalous light signature. As it eclipsed a faraway star, it caused an unanticipated dip in the amount of light reaching our telescopes. The dimming action occurred immediately before and after it crossed the star’s path, causing momentary confusion.
It turns out that Chariklo sports not one but two cosmic necklaces. Containing a good amount of frozen water, the larger of the rings hugging the planet is 7 kilometers (4 mi) wide, while the smaller is about half that size.
And while some asteroids do have “moons”—tiny satellites dancing around them—Chariklo is unique because a ring around an asteroid had never been observed. The rings’ origin is unclear, though it appears they were formed by an impact. They are either the remnants of a foreign body that shattered itself against Chariklo or pieces of Chariklo itself that blew off during the crash.

6UV Underproduction

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We pride ourselves on ascertaining the many universal balances that seem to occur throughout the cosmos. One such correlation has been observed between ultraviolet light and hydrogen, as the two have been found to coexist in well-defined proportions.
A recent survey, however, has thrown a monkey wrench into these suppositions and reported a severe underproduction of UV photons from known sources—a 400-percent discrepancy compared to predicted values. Lead author Juna Kollmeier likens it to walking into a dazzlingly bright room only to find several dim bulbs responsible for the disproportionate brilliance.
Two accepted processes produce UV radiation—unruly young stars and massive black holes—but more UV radiation exists than could have been produced by the two. Astronomers can’t explain the superfluous UV production and are forced to admit that “at least one thing we thought we knew about the present-day universe isn’t true.” That’s quite disheartening, considering that UV-hydrogen balance was believed to be very well understood. As in many times in the past, astronomers are forced back to the drawing board.
Quite mysteriously, this UV underproduction is only apparent at local distances. When looking farther off into space and time, astronomers find that their predictions hold up quite well. They’re remaining optimistic, though, since the unaccounted radiation could be the result of exotic, heretofore undiscovered processes. These possibly even involve dark matter decay.

5Weird X-rays

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Odd X-ray pulses are streaming from the core of the Andromeda and Perseus galaxies. And the signals’ spectrum (or light signature) does not match any known particle or atom. So astronomers are tentatively salivating over the prospect of a scientific breakthrough, as this phenomenon could just be the first tangible sign of dark matter.
Dark matter—the elusive, invisible bulk that accounts for most of the mass in the universe—might be composed of sterile neutrinos, which may or may not exist depending on whom you ask. These theorized particles supposedly produce X-rays in their death throes, and such emissions could account for the unexplained surges from the center of the aforementioned galaxies.
Furthermore, since the radiation emanates from the cores of the galaxies, it corresponds to areas of highly concentrated dark matter clumps. So while nothing is certain yet, this could be a momentous discovery that would greatly increase our understanding of a long-standing universal mystery.

4The Six-Tailed Asteroid

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Hubble has revealed yet another incredible curiosity—an asteroid that thinks it’s a comet. While the latter bodies are easily recognized by their bright, streaming tails, asteroids do not usually have such features since they possess little ice and are made mostly of heavier elements and rock. So spotting an asteroid with not one but six tails was an incredible surprise.
Asteroid P/2013 P5 is a unique find with its six spouting jets, as all other pieces of cosmic debris are quite content with considerably fewer. It blasts material indiscriminately into space like a cosmic lawn sprinkler
It’s unclear why the object behaves and looks the way it does. One awesomely destructive possibility is that P5 is rotating so quickly that it’sinadvertently killing itself. Its tiny gravity is no match for the greater rotational forces ripping it apart. And radiation pressure from solar emissions stretches the scattering debris into dazzling, comet-like appendages.
However, astronomers do know that P5 is a leftover chunk from a previous impact. The tails most likely contain zero ice content, since frozen water is unlikely to be found in an object that’s been previously exploded to 800 degrees Celsius (1,500 °F).

3HD 106906b, The Distant Monster

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Planet HD 106906b is a head-scratcher. This super-monster is 11 times more massive than Jupiter, and its gaping orbit highlights all sorts of flaws in our tenuous understanding of planetary formation. HD’s distance from its parent star is an absolutely mind-boggling 650 astronomical units (AU).
The incredibly lonely Neptune, our most distant planet, lumbers around the Sun at a distance of 30 AU. This is already an amazing range, but HD is so far separated from its parent that Neptune and the Sun are comparatively within hugging distance. This huge discrepancy is responsible for the addition of many asterisks above our planetary formation theories, as astronomers scramble to explain HD’s existence in spite of its vast orbit and heft.
For example, the forces responsible for making planets are usually undone by such great distances, raising the possibility that HD was created via the collapse of a debris ring. Yet HD is too massive for that to happen. And the primordial disks of raw matter that can birth planets simply do not contain enough stuff to produce giants like HD.
Another possibility is that we’ve discovered a failed binary star system, wherein HD failed to attract enough material to ignite fusion within its gassy bosom. However, the mass ratio between potential binaries is usually no more than 10:1. In HD’s case, however, we’re looking at a 100:1 disparity.

2Uranus Is Stormy

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Astronomers have been caught completely off guard by Uranus. The second-farthest member of our solar family is typically frigidly calm, but for some odd reason, the planet is currently awash in raging storms.
Dazzling Uranian tempests were expected back in 2007, during its equinox as the planet completed half of its 82-year orbit, and the full solar fury was unleashed directly upon the equator. Yet the stormy weather was supposed to abate as Uranus continued its journey around the Sun. It hasn’t.
With no internal heat source, the green giant relies on solar exposure to fuel its storms. But astronomers from the University of Berkeley, California recently observed major activity in the planet’s upper region, a vast layer of frozen methane. Some of these storms are close to the size of Earth, spiraling through the planet’s atmosphere for thousands of miles and shining so intensely that even amateur astronomers can spot large patches of light across the surface.
It’s unclear how the storms managed to stay healthy without the Sun’s assistance. The northern hemisphere has plunged into shadow yet still continues to host violent storm fronts. However, it’s possible that vortexesdeeper within the planet are caused by similar processes to those observed on the much more tumultuous Jupiter.

1KIC 2856960, The Triple-Star System

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Photo credit: M. Kornmesse/ESO
The Kepler Space Observatory is usually busy hunting down new planets, but it spent four years of its life tracking three gravitationally bound stars collectively known as KIC 2856960. KIC was just a run-of-the-mill triplet, two little dwarf stars orbited by a third stellar body going stag. Nothing weird so far, just three stars.
For example, Kepler saw four daily dips in the light curve as the binary dwarfs crossed each other every six hours. It also saw another slight decline in the observed light every 204 days caused by the eclipsing third star.
You’d think four years’ worth of observation would be enough to get well acquainted with KIC. And so did astronomers. But after fiddling with the numbers, the data didn’t make sense in the context of the observed behaviors of the stars. Their first job was to pin down the stellar masses. But no matter how they crunched the numbers, they failed to produce any sensible answers, even though ascertaining the mass of the stars should have been relatively straightforward.
For now, the stellar threesome has astronomers stumped. There is a potential answer that makes sense numerically yet not logically. It’s so farfetched to be almost unthinkable. The KIC system might contain a hidden fourth star. However, its orbit would have to perfectly mimic the orbit of the third star, giving the illusion of a single object.

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KVPY APPLICATION

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                                         KVPY


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PSLV (POLAR SATELLITE LAUNCH VEHICLE)

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                              PSLV LAUNCH VEHICLE INFORMATION               
                                      PSLV - The Polar Satellite Launch Vehicle is an Indian expendable launch system developed and operated by the Indian Space Research Organisation. The launch vehicle is a medium lift launcher that can reach a variety of orbits including Low Earth Orbit, Polar Sun Synchronous Orbit and Geosynchronous Transfer Orbit. PSLV is operated from the Satish Dhawan Space Center located in Sriharikota on India's East coast.

PSLV is a four-stage rocket that uses a combination of liquid fueled and solid fueled rocket stages. The vehicle can fly in three different configurations to adjust for mission requirements.

The Polar Satellite Launch Vehicle features six Strap-on Solid Rocket Boosters clustered around its first stage which itself is also solid-fueled. The second stage is liquid fueled while the third stage is a solid rocket motor. 
The Upper Stage of the PSLV uses liquid Propellant. The launcher stands 44.4 meters tall and has a diameter of 2.8 meters.  Depending on the launcher's configuration, PSLV weighs 229,000, 296,000 or 320,000 Kilograms.

In addition to the 'regular' PSLV version, it can fly in its Core Alone configuration, without the six Solid Rocket Boosters and less propellant in the tanks of its upper stage - a configuration used for missions that feature small payloads. PSLV can also fly in a XL Version that launches with additional propellant in its Solid Rocket Boosters to increase payload capability.

PSLV can deliver payloads of up to 3,250kg to Low Earth Orbit. Sun Synchronous capability is 1,600kg and Geosynchronous Transfer Orbit capability reaches 1,410 Kilograms.

PSLV was designed and developed by the Indian Space Research Organisation at the Vikram Sarabhai Space Center. PSLV made its first flight on September 20, 1993, but the mission failed early into flight when a large disturbance occurred at the point of second stage separation and one of the retro rockets of the second stage failed resulting an error in the flight control software of the vehicle. 
Picture
Photo: Indian Space Research Organisation
The vehicle fell back to Earth and crashed in the Bay of Bengal about 12 minutes after launch. The second flight of the launcher was performed 13 months later after modifications were made to the vehicle. PSLV D2 successfully achieved orbit, placing the IRS P2 Remote Sensing Satellite in a 820-Kilometer Sun Synchronous Orbit. One more successful development flight followed in 1996 before regular flights of the PSLV became available. The first operational flight of the vehicle came in 1997, but did send the IRS 1D payload into an elliptical orbit instead of a circular Sun Synchronous trajectory, requiring the satellite to perform orbit adjustments to meet its mission objectives. The flight was recorded as partial failure. 
This was the final failure of PSLV that has so far completed 21 operational flights with 20 successes.

Regular

Picture
Photo: Indian Space Research Organisation

Core Alone

Picture
Photo: Indian Space Research Organisation

PSLV-XL

Picture
Photo: Indian Space Research Organisation
TypePSLV
VersionsRegular, Core Alone, XL
Height44.5m
Diameter2.8m
Launch Mass229,000kg (CA) to 320,000kg (XL)
Mass to LEO3,250kg
Mass to GTO1,410kg
Mass to SSO1,600kg - XL: 1,800kg - CA: 1,100kg
Photo: Indian Space Research Organisation

First Stage

Picture
TypePS1
Inert Mass30,200kg
Launch Mass168,200kg
Diameter2.8m
Length20.34m
PropellantSolid - HTPB Based
Fuel Mass138,00kg
PropulsionPS1 Solid Rocket Motor
Thrust (Vacuum)4,860kN
Impulse269s
Burn Time105sec
Restart CapabilityNo
Attitude ControlSITVC (Pitch&Yaw), Roll RCS
Stage SeparationFlexible Linear Shaped Charge
 Separation Motors


Solid Rocket Boosters

# BoostersCA:0 - Regular&XL:6
Length10.0m (Regular), 13.5m (XL)
Diameter1.0m
Dry Mass2,010kg
Launch Mass11,000kg (Regular), 14,000kg (XL)
PropellantSolid - HTPB Based
Fuel Mass~9,000kg (Regular), ~12,000kg (XL)
Thrust (Vacuum)502.6kN
Burn Time44sec (Regular) 49.5sec (XL)
Impulse262s
Attitude ControlSITVC on two Boosters
Stage SeparationBall & socket joint, spring thruster
Picture
Photo: Indian Space Research Organisation


Second Stage

TypePS2
Diameter2.8m
Length12.8m
Inert Mass5,300kg
Launch Mass46,000kg
FuelUnsymmetrical Dimethylhydrazine
OxidizerNitrogen Tetroxide
Propellant Mass40,700kg
Propulsion1 Vikas
Thrust799kN
Impulse293s
Engine Dry Weight900kg
Burn Time158sec
Chamber Pressure58.5bar
Mixture Ratio1.7 (Ox/Fuel)
Area Ratio31
Prop Flow Rate278.04kg/s
Attitude ControlMain Engine Gimbaling, Roll RCS
Stage SeparationMerman Band, Sep Motors
Picture
Photo: Indian Space Research Organisation

Third Stage

TypePS3
Diameter2.02m
Length3.54m
Inert Mass1,100kg
Launch Mass7,800kg
Propellant Solid - HTTP Based
Propellant Mass6,700kg
PropulsionS-7
Thrust 244kN
Impulse294s
Burn Time112sec
Attitude Control4th Stage RCS
SeparationBall Lock


Fourth Stage

TypePS4
Diameter2.02m
Length2.60m
Inert Mass920kg
Launch Mass2,920kg (Regular, XL), 2,520kg (CA)
FuelMonomethylhydrazine
OxidizerMON3 (Mixed Oxides of Nitrogen)
Propellant Mass2,000kg (Regular, XL), 1,600kg (CA)
Propulsion2 L-2-5
Total Thrust 14.6kN
Impulse308s
Chamber Pressure8.4bar
Engine Diameter0.66m
Burn TimeVariable, Up to 525sec
Area Ratio60
Attitude controlReaction Control System
SeparationBall Lock


Payload Fairing

Diameter3.2m
Length8.3m
Mass1,150kg
SeparationPiston Cylinder Mechanism
 Clamp Band
ConstructionAluminum Alloy, Semi Monocoque
 Spherical Nose Cap, Forward
 Conical Section, Cylindrical Section,
 Conical Boat-tail
Picture
Photo: Indian Space Research Organisation

First Stage

The first stage of the PSLV, PS1, is a solid fueled rocket stage - one of the largest solid rockets ever flown, behind the Space Shuttle's Solid Rocket Boosters and the Ariane 5 EAPs. It is 20.34 meters long and 2.8 meters in diameter with an empty mass of 30,200 Kilograms. The stage contains 138,000kg of HTPB (Hydroxyl-terminated polybutadiene) bound propellant at liftoff. PS1 has a vacuum thrust of 4,860 Kilonewtons. 

First stage attitude control is provided by a  Secondary Injection Thrust Vector Control (SITVC) for yaw and pitch. For SITVC, Strontium Perchlorate is used as a secondary fluid that is injected from the side into the Hypersonic Flow in the nozzle, causing a lateral thrust element that is precisely steered for attitude control. The SITVC fluid is stored in  two cylindrical aluminum tanks strapped to the core stage. The tanks are pressurized with Nitrogen. Roll control is provided by two Roll Control Thrusters that are mounted radially on opposite sides of the core stage between the Solid Rocket Boosters. 

The first stage burns for 105 seconds and is separated at an altitude of 76 Kilometers by a flexible linear shaped charge. Separation motors are used to ensure the first stage moves away from the second stage before it ignites.
Picture
Photo: Indian Space Research Organisation

Solid Rocket Boosters

PSLV in its standard and XL configuration uses six Solid Rocket Boosters, four are ignited on the ground and two boosters are air-lit. Each of the standard PSOM boosters has an empty mass of 2,010 Kilograms, is 1.0 meter in diameter and has a length of 10.0 meters. The boosters use nearly 9,000 Kilograms of HTPB propellant to provide a vacuum thrust of 503 Kilonewtons for a total burn time of 44 seconds. Two of the boosters of the vehicle have an SITVC system to provide roll control augmentation. The two air-lit boosters are usually ignited 25 seconds into the flight.

In the PSLV XL configuration, the PSOM-XL boosters are stretched to accommodate additional propellant for a longer burn time. PSOM-XL is 13.5 meters long and contains 12,000 Kilograms of solid propellant. The XL boosters have a burn time of 49.5 seconds.


The ground-lit Boosters separate at T+68 seconds at an altitude of 24 Kilometer while the air-lit boosters are jettisoned at T+90 seconds at an altitude of 41 Kilometers.
Picture
Photo: Indian Space Research Organisation

Second Stage

The second stage of the PSLV rocket is 2.8 meters in diameter, 12.8 meters long and has a liftoff mass of 46,000 Kilograms with an empty mass of 5,300 Kilograms. The stage uses Unsymmetrical Di-Methylhydrazine / Hydrazine Hydrate as fuel and Nitrogen Tetroxide as oxidizer. It is powered by a single 799-Kilonewton Vikas engine. Vikas was developed by ISRO in the 1970s. 




The engine has a dry weight of 900 Kilograms and operates at a chamber pressure of 58.5 bar and provides a specific impulse of 294 sec. The second stage burns for 158 seconds. Vehicle control during second stage flight is accomplished by gimbaling the main engine by up to 4 degrees, roll control is provided by a Hot Gas Reaction Control Motor.

Second stage separation is accomplished with a merman band system and separation motors. It occurs at an altitude of 277 Kilometers.

Third Stage

The PS3 stage is a solid rocket motor that also uses an HTPB based propellant. The third stage of the PSLV launcher has a reduced diameter of 2.02 meter and a length of 3.54 meters. It has an empty mass of 1,100 Kilograms and a liftoff weight of up to 7,800 Kilograms. The stage has a burn time of 112 seconds during which it generates a thrust of 244 Kilonewtons. The stage has  a Kevlar-polyamide fiber case and a submerged nozzle equipped with a flex-bearing-seal gimbaled nozzle that can be gimbaled by up to 2 degrees for Thrust Vector Control. Roll control is provided by the Reaction Control System of the fourth stage. The third stage separates at an altitude of of 580 Kilometers.

Fourth Stage

The Upper Stage of the PSLV launcher is liquid fueled using Monomethylhydrazine fuel and Mixed Oxides of Nitrogen as an oxidizer. The stage is 2.02 meters in diameter and has a length of 2.60 meters with an empty mass of 920 Kilograms. It contains 2,000 Kilograms of propellant when flying on the regular and XL configuration and 1,600 Kilograms when flying atop the CA configuration. The fourth stage is powered by two L-2-5 engines, each producing a thrust of 7.4kN and a specific impulse of 309 sec. The engines can be gimbaled by up to 3 degrees for pitch and yaw control while roll control is provided by the Reaction Control System. The RCS is also used during coast periods and to re-orient the vehicle for spacecraft separation. The fourth stage has a variable burn time depending on the mission profile. It can support burns of up to nine minutes. 

The fourth stage also houses the Equipment Bay of the vehicle containing the inertial guidance system and flight computer (Vikram 1601) as well as telemetry and avionics equipment.
Picture
Photo: Indian Space Research Organisation

Payload Fairing

The Payload Fairing, or "Heat Shield" as ISRO refers to it, is positioned on top of the stacked vehicle and its integrated Payload. It protects the spacecraft against aerodynamic, thermal and acoustic environments that the vehicle experiences during atmospheric flight. When the launcher has left the atmosphere, the fairing is jettisoned by pyrotechnical initiated systems. Separating the fairing as early as possible increases launcher performance.

The typical PSLV Payload Fairing is 3.2 meters in diameter, 8.3 meters long and weighs 1,150 Kilograms. It consists of two all-aluminum halves that consist of different section. On top, the fairing has a spherical nose cone and a conical section at the forward end. A long cylindrical and a short conical boat-tail follow. The conical sections are stiffened semi-monocoque structures and the cylindrical section is and integrally stiffened isogrid structure made up of three 1.5-meter panels.

The payload fairing features a controlled environment and Payload purge supply as well as acoustic absorption blankets. Additionally, the fairing can be outfitted with RF windows.

The fairing is separated about 165 seconds into the flight at an altitude of 130 Kilometers. Separation is accomplished by a linear piston cylinder separation and jettisoning mechanism (zip cord) running along the full length of the PLF and a clamp and joint at the base of the fairing. Both systems are pyrotechnically initiated. The gas pressure generated by the zip cord expands a rubber bellow that pushes that piston and cylinder apart, pushing the fairing halves laterally away from the launcher.

Payload Adapter

Payload Adapters interface with the vehicle and the payload and are the only attachment point of the payload on the Launcher. They provide equipment needed for spacecraft separation and connections for communications between the Upper Stage and the Payload. 

The adapters feature the traditional clamp-band separation system, but low-shock options are available as well. The adapter is located on top of the fourth stage and Vehicle Equipment Bay. A number of standard adapters are available to accommodate a number of payloads, but payloads adapters can also be custom-built based on special payload requirements.

Auxiliary Payloads

PSLV is capable of carrying a number of secondary payloads into orbit via payload dispensers mounted on the vehicle equipment bay. These dispensers can either hold two satellites in the mass range of 50 to 150kg or more smaller satellites being released by small satellite deploying mechanisms. VEB is an annular deck plate made of Aluminium honeycomb panels, and mounted around the propellant tank of the Fourth Stage. Two plates are are installed on the VEB that serve as installation points for the payload accommodations that are located 180 degrees apart. 
P.S:NOTE: BEFORE INVENTION OF PSLV BY INDIA ..THE TECHNOLOGY WAS AVAILABLE ONLY IN RUSSIA..INDIANS ON ACCOUNT OF THEIR TIRELESS TOIL GIVE CEASELESS AMUSEMENT TO THE WORLD AND ARE YET TO UNFOLD THE GREATEST TECHNOLOGIES..
         
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Vehicle Configurations

Specifications


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