SPACE VEHICLE - PSLV & GSLV - Space ORBITS

SPACE VEHICLE - PSLV & GSLV - Space ORBITS (S&T) GS PAPER-3

India has one of the world's most effective and active space programmes, with a diverse set of missions and accomplishments in the space sector. The Indian Space Research Organisation (ISRO) is India's primary space agency located in Bangalore. It has made significant contributions in areas such as satellite launch technology, remote sensing, and space exploration, from launching its very first satellite in 1975.

Different Types of Satellite Orbits:

Geosynchronous orbit:

• It is a path around the Earth where the orbital period matches the Earth’s rotation period.
• This path in high Earth orbit(as it is placed at an altitude of 35790 km) is known as a geosynchronous orbit.
• Telecommunications and remote sensing satellites are placed in this orbit.

Geostationary Orbit (GSO):

• It is a geosynchronous orbit with an inclination of zero, i.e. it lies on the same plane as that of the equator. It lies 35,786 km above earth’s equator.
• A satellite in this orbit appears to be stationary as seen from the earth. The geostationary satellite remains at the same position throughout the day.
• Thus, it is used for applications which requires a direct line of communication between the satellite and the receiver(for example-direct tv broadcast).

Geosynchronous Transfer Orbit:

• Geostationary transfer orbit is a temporary orbit. It is an elliptical orbit at a height of 35,786 km.
• Its inclination is nearly the same as the latitude of the location from where a spacecraft is launched.
• It is used to transfer a spacecraft from a low altitude orbit or flight trajectory to geosynchronous or geostationary orbit.

Semi-synchronous orbit :

• It is a path around the Earth where the orbital period is 12 hours.
• These orbits are at a height of 20,200 km(medium-earth orbit/MEO) above the earth’s surface.
• These are near circular orbits and Global Positioning System (GPS) satellites are placed in these orbits.

Polar orbits:

• Polar orbits are the ones that pass over the Earth from its north pole to the south pole. These orbits mainly take place at low altitudes of between 200 and 1000 km.
• It usually takes around one and a half hours for one rotation. For a satellite in a polar orbit, the earth is rotating below it.
• Thus, it can cover the whole earth in 24 hours. They are used to monitor crops, remote sensing etc.

Sun synchronous Orbits:

• These are polar orbits are synchronous with the Sun. Thus, it passes over the same part of the earth at the same time of the day.
• A satellite in a sun synchronous orbit are usually at an altitude of between 600 and 800 km. Weather monitoring and spy satellites are usually placed in this orbit.

Low Earth Orbit:

• A low Earth orbit is normally at an altitude of less than 1000 km.

Earth Parking Orbit:

• An Earth parking Orbit is a temporary orbit used during the launch of a satellite before the satellite being boosted into its final orbit.

Launch Vehicle

Satellite Launch vehicles are the bedrock of space missions and satellite deployment in space. The satellite missions rely on powerful launch vehicles, also known as rockets, to carry satellites and payloads into space.

• ISRO's journey into satellite launch vehicles began with the SLV, India's first experimental satellite launch vehicle, in 1980, and later with a more advanced Augmented Satellite Launch Vehicle.
• In 1994, ISRO launched its first PSLV and in 2001, ISRO further advanced the launch vehicle technology to build GSLV, which can take more heavy satellites in the Geosynchronous and Geostationary Orbit.

Sounding rockets

Are one- or two-stage solid-propellant rockets employed to explore the upper atmosphere as well as carry out space research. Sounding rockets enabled the use of rocket-borne instrumentation to probe the atmosphere in situ.

• The first rockets were two-stage Russian (M-100) and French (Centaure) rockets. ISRO began launching indigenously built sounding rockets in 1965.
• The first sounding rocket was launched in 1963 from Thumba near Thiruvananthapuram, marking the beginning of the Indian Space Programme.
• The Rohini Sounding Rocket (RSR) Programme consolidated all sounding rocket activities in 1975.
• Currently, three operational sounding rocket versions are available, with payloads ranging from 8 to 100 kg and apogees ranging from 80 to 475 km.

Polar Satellite Launch Vehicle (PSLV)

• It is India's third-generation launch vehicle, first successfully launched in October 1994. It is the first Indian launch vehicle to have liquid stages.
• It is a four-stage vehicle with multiple satellite launch capabilities and multiple orbit capabilities.

• PSLV-XL, QL, and DL variants use 6,4,2 solid rocket strap-on motors to supplement the thrust provided by the first stage.
  • Strap-ons, on the other hand, are not used in the core-alone version of PSLV (PSLV-CA).
• Due to PSLV's unmatched reliability, numerous satellites, including satellites from the IRNSS constellation, have been launched into geosynchronous and GEO.
  • Thus, it is regarded as “the workhorse of ISRO” for Low Earth Orbits (LEO).
• Payload capacity: It can carry up to 1,750 kg of payload to 600 km altitude Sun-Synchronous Polar Orbits.
• Numerous Indian and foreign customer satellites have been launched by PSLV.
  • It successfully launched Chandrayaan-1 in 2008 and Mars Orbiter Spacecraft in 2013.

Geosynchronous Satellite Launch Vehicle (GSLV)

• It is a 4th generation launch vehicle designed to place communication satellites in geostationary transfer orbit using a cryogenic third stage. It was used for launching Chandrayaan-2.
• It is a three-stage vehicle with four liquid strap-ons. Initially, cryogenic stages from Russian GK were used; later, it was developed indigenously.

• Payload capacity: GSLV is capable of placing up to 6 tonnes of payloads in Low Earth Orbits, from heavy satellites to multiple smaller satellites.
  • Further, it is capable of putting a 2,250 kg satellite into Geosynchronous Transfer Orbit (GTO), such as the INSAT and GSAT communication satellites.
• GSLV with indigenous Cryogenic Upper Stage made possible the launch of communication satellites weighing up to 2 tonnes.
  • In comparison to solid and earth-storable liquid propellant rocket stages, a cryogenic rocket stage is more efficient and provides more thrust per kilogramme of propellant burned.

LVM3 (Geosynchronous Satellite Launch Vehicle Mk III)

It is a next-generation launch vehicle of ISRO. Previously it was known as Geosynchronous Satellite Launch Vehicle Mk III (GSLV MkIII).

It is a three-stage vehicle with two solid strap-on motors, one liquid core stage and a high-thrust cryogenic upper stage.

Payload capacity: It is capable of putting the GSAT series' 4-tonne satellites into Geosynchronous Transfer Orbits.

LVM3's powerful cryogenic stage allows it to place payloads of up to 8000 kg into 600 km Low Earth Orbits. Recently, it was used for launching the Chandrayaan-3 mission.

Under Development

ISRO has been advancing its technology to build new satellites according to the need and future prospects such as space stations, manned missions and the launching of small satellites. Following are the satellite launch vehicles of ISRO under development:

• Human Rated Launch Vehicle (HRLV):
  • It will be the modified version of the current heavy-weight LVM-3 launch vehicle.
    • It will be capable of launching the Orbital Module into a 400 km Low Earth Orbit.
  • It will include a Crew Escape System (CES) powered by quick-acting and high-burn rate solid motors.
• Small Satellite Launch Vehicle (SSLV):
  • It is a three-stage launch vehicle with three solid propulsion stages and a terminal stage based on liquid propulsion called the Velocity Trimming Module.
  • It is capable of launching nano, micro and mini satellites up to 500 kg satellite in a 500km planar orbit.
• Reusable Launch Vehicle - Technology Demonstrator (RLV-TD):
  • The RLV-TD's configuration resembles that of an aircraft because it combines the complexity of launch vehicles and aeroplanes.
  • It comprises a nose cap, a fuselage (body), two delta wings, and two vertical tails. Elevons and Rudder, which are symmetrically placed active control surfaces, are also included.
  • In future, it will be scaled up to become the first stage of India’s reusable two-stage orbital launch vehicle.
  • SpaceX has the Falcon 9, one of the most important heaviest reusable launch vehicle.
• Scramjet Engine - TD:
  • A scramjet engine outperforms a ramjet engine by operating at hypersonic speeds and allowing supersonic combustion. The engine uses Hydrogen as fuel and Oxygen from the atmospheric air as the oxidiser.
  • The first experimental mission of the Scramjet Engine towards the realisation of an Air Breathing Propulsion System was successfully conducted in 2016 by ISRO.
  • India is the fourth country to demonstrate the flight testing of a Scramjet Engine.

Notable Foreign Launch Vehicles

The ISRO has utilised various foreign launch vehicles for launching satellites. Some of the notable foreign launch vehicles are given below:

• Arien 5: It is one of the heavy-lift launchers used by European Space Agency. It is capable of carrying payloads weighing more than 20 metric tons into LEO and over 10 metric tons to geostationary transfer orbit. India has used Arien 5 launch vehicles for launching manby communication and earth observation satellites such as INSAT-3D and GSAT 30.
• Falcon 9: It is the world's first orbital class reusable rocket with two-stages designed and manufactured by SpaceX. It is capable of launching payload of 22 metric tonnes to the Low Earth Orbit and 8 metric tonnes to Geostationary orbit.
• Space Launch System (SLS): It is a super heavy-lift rocket developed by NASA. It is capable of launching a payload of 70 metric tonnes to LEO.
  • It is the only rocket capable of transporting the Orion spacecraft, four astronauts, and large cargo to the Moon in a single mission.
  • It includes both crew and service modules and a launch abort system.
• Soyuz 5: It is one of heaviest launch vehicle of the Russian Space Agency, with capability of launching 17 metric tonnes to the LEO.