PSLV-C61 Mission and the EOS-09 Satellite

PSLV-C61 Mission and the EOS-09 Satellite

23-05-2025
  1. ISRO launched the PSLV-C61 mission on May 18, 2025, aiming to place the EOS-09 satellite into a Sun-Synchronous Polar Orbit.
    • A Sun-Synchronous Polar Orbit (SSO) is a specific type of polar orbit where a satellite maintains a consistent relationship with the Sun.
    • This means the satellite always passes over a given point on Earth's surface at the same local time. SSOs are also known as helio-synchronous orbits.

  1. The mission failed due to a malfunction in the 3rd stage of the rocket.
  2. ISRO Chairman V. Narayanan confirmed that the failure was caused by a sudden drop in chamber pressure in the 3rd -stage solid motor casing.


What is PSLV?

 

  1. PSLV stands for Polar Satellite Launch Vehicle.
  2. It is an indigenously developed four-stage expendable rocket system by ISRO.
  3. The PSLV is referred to as the "Workhorse of ISRO" due to its high success rate and operational reliability.

 

Legacy of PSLV

  1. The PSLV achieved its first successful launch in October 1994.
  2. It is known for launching multiple satellites in a single mission, often serving both domestic and foreign clients.
  3. It Launches remote sensing, meteorological, navigation, communication, and scientific research satellites.
  4. Notable missions:
    • Chandrayaan-1 (Moon, 2008)
    • Mars Orbiter Mission (Mangalyaan) (2013)
    • Aditya-L1 (Sun, 2023)
    • Astrosat (India’s first space observatory)

Key Technical Specifications of PSLV-XL

Feature

Details

Stages

4 (Solid-Liquid-Solid-Liquid)

Lift-off Mass (XL variant)

Up to 320 tonnes

Payload to SSPO (600 km)

~1,750 kg

Payload to Sub-GTO

~1,425 kg

Total Height

~44 meters

Launch Site

Satish Dhawan Space Centre, Sriharikota

Stage-wise Description of PSLV

  1. Stage 1 (PS1) uses solid HTPB propellant and provides the initial thrust. It includes 6 strap-on boosters in the XL configuration.
  2. Stage 2 (PS2) uses a liquid Vikas engine, powered by UDMH and N2O4, and operates after atmospheric exit.
  3. Stage 3 (PS3) is a solid propellant stage using HTPB, designed to provide high thrust. This was the stage that failed in the C61 mission.
  4. Stage 4 (PS4) is a liquid stage powered by two engines using MMH and MON. It is restartable and responsible for final satellite insertion.
     

What is EOS-09 Satellite

  1. The EOS-09 is an Earth Observation Satellite designed for high-resolution remote sensing.
  2. It supports various civilian applications including agriculture, water resource monitoring, urban planning, and disaster response.
  3. It was intended to be deployed in a 600 km Sun-Synchronous Polar Orbit to ensure consistent lighting conditions.
     

PSLV Variants and Configurations

Variant

Description

Strap-on Boosters

Payload to SSPO

PSLV-CA (Core Alone)

No strap-ons; used for lighter payloads

None

~1,019 kg

PSLV-G

Standard with 6 boosters

6

~1,600+ kg

PSLV-XL

Extended; high capacity

6 (XL type)

~1,750 kg

PSLV-DL

Dual booster config

2

~1,200–1,300 kg

PSLV-QL

Quick launch, 4 boosters

4

~1,523 kg

Comparison: PSLV (Polar Satellite Launch Vehicle) and GSLV (Geosynchronous Satellite Launch Vehicle)
 

  1. The PSLV and GSLV are both used by India to launch satellites, but they have different capabilities and purposes.
  2. PSLV is primarily used for launching Earth observation and remote sensing satellites into lower orbits, while GSLV is designed for launching heavy communication satellites into Geosynchronous Transfer Orbit (GTO).
  3. GSLV also utilizes a cryogenic stage, which PSLV does not, for more powerful launches.

     

Feature

PSLV

GSLV

Number of Stages

4

3

Propulsion Type

Solid and Liquid

Liquid and Cryogenic

Lift-off Mass

Approximately 320 tonnes

Approximately 420 tonnes

Primary Orbit Type

SSPO and Low Earth Orbit

GTO and High Earth Orbit

Maximum Payload

~1.75 tonnes (SSPO)

~2.25 tonnes (GTO)

Key Missions

Earth Observation and Scientific

Communication and Heavy Payloads

Notable Variants

CA, G, XL, DL, QL

Mk I, Mk II, Mk III

Implications of PSLV-C61 Failure

  1. The PSLV-C61 failure is a rare setback in PSLV’s largely successful record.
  2. It highlights the technical complexity of multi-stage launches, especially with solid propulsion systems.
  3. ISRO’s quick diagnosis and public communication indicate transparency and institutional resilience.
  4. The relaunch of EOS-09 will be crucial for maintaining confidence in the PSLV’s reliability.
     

Strategic Importance of PSLV

  1. The PSLV has played a critical role in India’s space diplomacy, launching satellites for over 30 countries.
  2. It has enabled India to become a low-cost, reliable launch partner in the global space market.
  3. Despite occasional failures, the PSLV continues to be central to ISRO’s scientific and strategic missions.
     

Conclusion

The PSLV remains a cornerstone of India’s space program, known for its versatility, cost-effectiveness, and proven performance. The PSLV-C61 failure underscores the importance of continuous innovation and rigorous quality control. ISRO’s response demonstrates its maturity as a scientific organization, and the upcoming reattempt of EOS-09 will be an opportunity to reaffirm PSLV's legacy.

 

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