हिन्दी
About ISRO Propulsion Complex (IPRC)
Overview The ISRO Propulsion Complex (IPRC), situated on the lower slopes of the Mahendragiri hills in Tamil Nadu, is a premier centre of excellence dedicated to the assembly, integration, and testing of liquid propulsion systems for India’s launch vehicles and spacecraft. Spanning an expansive area of nearly 6,400 acres, IPRC provides a world-class platform for validating the entire spectrum of liquid rocket technology, contributing significantly to the success of every major ISRO mission.
Core Mandate IPRC is entrusted with the executive mandate to realize propulsion power plants with thrust capacities ranging from 2 kN to 2000 kN. This encompasses:
• System Realization: The assembly and delivery of Earth-storable, cryogenic, and semi-crygenic engines and stages for operational launch vehicles, including PSLV, GSLV, and LVM3.
• Rigorous Validation: Conducting developmental, qualification, and flight acceptance testing of engines and stages under both sea-level and High Altitude (HAT) simulated space environments.
• Propellant Management: Serving as a critical hub for the production and supply of cryogenic propellants (Liquid Hydrogen, Liquid Oxygen, and Liquid Nitrogen) and storable liquid propellants for national launch and satellite programmes.
• System Realization: The assembly and delivery of Earth-storable, cryogenic, and semi-crygenic engines and stages for operational launch vehicles, including PSLV, GSLV, and LVM3.
• Rigorous Validation: Conducting developmental, qualification, and flight acceptance testing of engines and stages under both sea-level and High Altitude (HAT) simulated space environments.
• Propellant Management: Serving as a critical hub for the production and supply of cryogenic propellants (Liquid Hydrogen, Liquid Oxygen, and Liquid Nitrogen) and storable liquid propellants for national launch and satellite programmes.
Historical Evolution Established in 1982 as LPSC Mahendragiri to support the burgeoning needs of the Indian space programme, the centre has evolved from a testing facility into a multidisciplinary complex. In recognition of its expanding role and the strategic importance of liquid and cryogenic propulsion, the centre was elevated to its current status as ISRO Propulsion Complex (IPRC) on 1 February 2014. Since its inception, IPRC has reached significant milestones, from the first successful hot test in 1985 to propelling the Chandrayaan-3 mission and qualifying engines for the prestigious Gaganyaan human spaceflight programme.
Innovation and Strategic Vision IPRC is driven by a commitment to the "zero-defect" demand of the Indian space programme, ensuring the highest standards of safety, quality, and reliability. Beyond operational support, the complex actively pursues Strategic Research & Development (R&D) and Technology Development Programmes (TDP) to pioneer future-ready solutions. Current strategic focuses include:
• Next-Generation Propulsion: Development of the high-thrust 2000 kN Semi-cryogenic engine and the exploration of eco-friendly green propellants.
• Global Leadership: Fostering collaborations with private entities and research organisations to advance space technology and strengthen India’s position as a global leader in the space arena.
• Next-Generation Propulsion: Development of the high-thrust 2000 kN Semi-cryogenic engine and the exploration of eco-friendly green propellants.
• Global Leadership: Fostering collaborations with private entities and research organisations to advance space technology and strengthen India’s position as a global leader in the space arena.
IPRC Activities
The ISRO Propulsion Complex (IPRC) serves as the multidisciplinary hub for the propulsion lifecycle of the Indian space programme. Its activities encompass a wide spectrum of rocket technology, ranging from the intricate assembly of sub-systems to the rigorous validation of massive launch vehicle stages under simulated space conditions.
I. Propulsion System Realisation: Assembly and Integration
IPRC is mandated with the assembly, integration, and deliveryof propulsion power plants for liquid stages, covering a vast thrust spectrum from 2 kN to 2000 kN.
• Engine Assembly (EAIE): This entity meticulously assembles intricate sub-systems, including turbo pumps, for Earth-storable, cryogenic, and semi-cryogenic engines. It manages specialized facilities for throat bonding, protective coating, and rotor balancing to ensure the integrity of engines like the Vikas and CE20.
• Stage Integration (SAIE): IPRC is responsible for the realization of flight-worthy stages for the PSLV, GSLV, and LVM3 launch vehicles. This includes the vertical and horizontal integration of stages such as the PS2, GS2, L110, and C25, alongside developmental stages like the SC120.
• Precision Fabrication: The complex operates advanced fabrication facilities, including robotic plasma coating and orbital TIG welding, to ensure the high-precision realization of cryogenic and semi-cryogenic hardware.
IPRC is mandated with the assembly, integration, and deliveryof propulsion power plants for liquid stages, covering a vast thrust spectrum from 2 kN to 2000 kN.
• Engine Assembly (EAIE): This entity meticulously assembles intricate sub-systems, including turbo pumps, for Earth-storable, cryogenic, and semi-cryogenic engines. It manages specialized facilities for throat bonding, protective coating, and rotor balancing to ensure the integrity of engines like the Vikas and CE20.
• Stage Integration (SAIE): IPRC is responsible for the realization of flight-worthy stages for the PSLV, GSLV, and LVM3 launch vehicles. This includes the vertical and horizontal integration of stages such as the PS2, GS2, L110, and C25, alongside developmental stages like the SC120.
• Precision Fabrication: The complex operates advanced fabrication facilities, including robotic plasma coating and orbital TIG welding, to ensure the high-precision realization of cryogenic and semi-cryogenic hardware.
II. Comprehensive Testing and Validation
As the primary testing hub for ISRO, IPRC conducts developmental, qualification, and flight acceptance testing for various propulsion systems.
• Static Fire Testing: The complex manages world-class test stands, such as the Principal Test Stand (PTS), capable of testing engines and stages up to 135 tonnes, including the human-rated Vikas engines for the Gaganyaan mission.
• High Altitude Testing (HAT): IPRC operates specialized facilities to simulate the vacuum of space, essential for qualifying upper-stage engines like the PS4 and spacecraft thrusters like the Liquid Apogee Motor (LAM).
• Semi-Cryogenic Validation: The newly commissioned Semi-Cryo Integrated Engine Test Facility (SIET) enables the testing of high-thrust 2000 kN engines using Isrosene and Liquid Oxygen, a critical milestone for future heavy-lift capabilities.
As the primary testing hub for ISRO, IPRC conducts developmental, qualification, and flight acceptance testing for various propulsion systems.
• Static Fire Testing: The complex manages world-class test stands, such as the Principal Test Stand (PTS), capable of testing engines and stages up to 135 tonnes, including the human-rated Vikas engines for the Gaganyaan mission.
• High Altitude Testing (HAT): IPRC operates specialized facilities to simulate the vacuum of space, essential for qualifying upper-stage engines like the PS4 and spacecraft thrusters like the Liquid Apogee Motor (LAM).
• Semi-Cryogenic Validation: The newly commissioned Semi-Cryo Integrated Engine Test Facility (SIET) enables the testing of high-thrust 2000 kN engines using Isrosene and Liquid Oxygen, a critical milestone for future heavy-lift capabilities.
III. Strategic Propellant Management and Production
IPRC plays a pivotal role in the Indian cryogenic rocket programme by managing the entire supply chain of high-energy propellants.
• Cryogenic Production: The complex operates the Liquid Hydrogen Production Plant,ensuring a sustainable supply of hundreds of tonnes of Liquid Hydrogen (LH2), Liquid Oxygen (LOX), and Liquid Nitrogen (LIN).
• Storage and Servicing: It is responsible for the analysis, storage, and uninterrupted supply of both cryogenic and Earth-storable liquid propellants for national launch vehicle and satellite programmes.
IPRC plays a pivotal role in the Indian cryogenic rocket programme by managing the entire supply chain of high-energy propellants.
• Cryogenic Production: The complex operates the Liquid Hydrogen Production Plant,ensuring a sustainable supply of hundreds of tonnes of Liquid Hydrogen (LH2), Liquid Oxygen (LOX), and Liquid Nitrogen (LIN).
• Storage and Servicing: It is responsible for the analysis, storage, and uninterrupted supply of both cryogenic and Earth-storable liquid propellants for national launch vehicle and satellite programmes.
IV. Strategic R&D and Technology Development
To maintain India's competitive edge, IPRC aggressively pursues Technology Development Programmes (TDP) and strategic research.
• Future Propulsion: Development of LOX-Methane systems and green propellants to create eco-friendly, sustainable rocket engines for the next generation of space exploration.
• Indigenous Automation: The complex has pioneered the development of indigenous Hot-Standby PLCs with a very low cycle time to replace imported systems, enhancing the safety and reliability of automated test sequences.
• Interplanetary Simulation: IPRC provides a specialized platform for simulation trials intended for interplanetary missions, including crucial ground tests for the Mars Orbiter Mission (MOM) and Chandrayaan modules.
To maintain India's competitive edge, IPRC aggressively pursues Technology Development Programmes (TDP) and strategic research.
• Future Propulsion: Development of LOX-Methane systems and green propellants to create eco-friendly, sustainable rocket engines for the next generation of space exploration.
• Indigenous Automation: The complex has pioneered the development of indigenous Hot-Standby PLCs with a very low cycle time to replace imported systems, enhancing the safety and reliability of automated test sequences.
• Interplanetary Simulation: IPRC provides a specialized platform for simulation trials intended for interplanetary missions, including crucial ground tests for the Mars Orbiter Mission (MOM) and Chandrayaan modules.
V. Advanced Engineering Support and Reliability
Every activity at IPRC is underpinned by a commitment to the "zero-defect" mandate.
• Quality Assurance (SRSE): The complex utilizes advanced Non-Destructive Testing (NDT), including high-energy X-ray imaging of internal engine structures.
• Metrology and Material Testing: Specialized labs provide precision dimensional inspections and cryogenic material testing, ensuring that every component can withstand the extreme thermal and structural loads of spaceflight.
Every activity at IPRC is underpinned by a commitment to the "zero-defect" mandate.
• Quality Assurance (SRSE): The complex utilizes advanced Non-Destructive Testing (NDT), including high-energy X-ray imaging of internal engine structures.
• Metrology and Material Testing: Specialized labs provide precision dimensional inspections and cryogenic material testing, ensuring that every component can withstand the extreme thermal and structural loads of spaceflight.
IPRC Facilities
IPRC operates a vast, world-class infrastructure spanning nearly 6,400 acres at Mahendragiri, specifically designed for the assembly, integration, and rigorous validation of India’s liquid propulsion systems. These facilities are engineered to the highest international standards, ensuring that every component—from small thrusters to massive 2000 kN engines.
I. Assembly and Integration Facilities
IPRC houses specialized environments for the meticulous realization of rocket engines and launch vehicle stages.
• Engine Assembly & Integration: These facilities feature Class 100,000 clean rooms with specialized tools and EOT cranes to ensure contaminant-free environments for mission-critical hardware dedicated to the assembly of intricate sub-systems, including turbopumps and thrust chambers for Earth-Storable, Cryogenic and Semi-Cryogenic engines. Specialized infrastructure includes:
• Specialised Sub-system Infrastructure: Facilities include Dynamic Balancing for rotors, Throat Fixing and Bonding: Controlled environments for curing refractory cement in engine throats, Plasma Coating for thermal barrier application on thrust chambers, and Water Flow Test facilities for the hydraulic characterisation of injectors and control valves
• Stage Assembly & Integration: These facilities manage the vertical and horizontal integration of flight-worthy stages (Earth-Storable, Cryogenic and Semi-Cryogenic Stages). Horizontal Integration Fixture used as a precise mechanism to align and integrate stages without straining the hardware. Insulation Processing Facility is a specialized bay for applying composite thermal insulation layers to cryogenic propellant tanks.
IPRC houses specialized environments for the meticulous realization of rocket engines and launch vehicle stages.
• Engine Assembly & Integration: These facilities feature Class 100,000 clean rooms with specialized tools and EOT cranes to ensure contaminant-free environments for mission-critical hardware dedicated to the assembly of intricate sub-systems, including turbopumps and thrust chambers for Earth-Storable, Cryogenic and Semi-Cryogenic engines. Specialized infrastructure includes:
• Specialised Sub-system Infrastructure: Facilities include Dynamic Balancing for rotors, Throat Fixing and Bonding: Controlled environments for curing refractory cement in engine throats, Plasma Coating for thermal barrier application on thrust chambers, and Water Flow Test facilities for the hydraulic characterisation of injectors and control valves
• Stage Assembly & Integration: These facilities manage the vertical and horizontal integration of flight-worthy stages (Earth-Storable, Cryogenic and Semi-Cryogenic Stages). Horizontal Integration Fixture used as a precise mechanism to align and integrate stages without straining the hardware. Insulation Processing Facility is a specialized bay for applying composite thermal insulation layers to cryogenic propellant tanks.
II. Propulsion Test Stands and Static Fire Facilities
IPRC serves as ISRO’s primary testing hub, featuring a suite of vertical and horizontal test stands capable of simulating both sea-level and vacuum conditions.
• Principal Test Stand (PTS): A robust facility capable of testing earth-storable engines and stages up to 135 tonnes, including nominal and off-nominal qualification tests for the Gaganyaan mission.
• Cryogenic Test Facilities (CTE): A cluster of sophisticated test stands for the CUS and CE20 projects:
o Main Engine & Stage Test (MET): A vertical facility for hot tests of cryogenic engines (up to 216 kN) and integrated stages.
o Thrust Chamber Test (TCT): Primarily used for pressure-fed developmental tests and high-altitude (HAT) flight acceptance of CE20 engines.
o Subscale Engine Test (SET): The pioneering cryogenic facility at IPRC, used for testing steering engines and turbopump sub-systems.
o Redundant and Upcoming Infrastructure: To increase throughput, IPRC has commissioned the Cryogenic Turbo-Pump Test (CTPT) facility and is realizing the Integrated Cryo Engine & Stage Test (ICET) facility, a mammoth 42-metre tall structure
• Semi-Cryogenic Integrated Engine & Stage Test (SIET): A state-of-the-art facility featuring twin test bays for the development of high-thrust 2000 kN semi-cryogenic engines using Isrosene and Liquid Oxygen.
• High Altitude Test (HAT) Facilities: Specialized vacuum environments (LUS-TF, STTF, and NLTF) used to qualify upper-stage engines like the PS4 and spacecraft thrusters like the Liquid Apogee Motor (LAM).
IPRC serves as ISRO’s primary testing hub, featuring a suite of vertical and horizontal test stands capable of simulating both sea-level and vacuum conditions.
• Principal Test Stand (PTS): A robust facility capable of testing earth-storable engines and stages up to 135 tonnes, including nominal and off-nominal qualification tests for the Gaganyaan mission.
• Cryogenic Test Facilities (CTE): A cluster of sophisticated test stands for the CUS and CE20 projects:
o Main Engine & Stage Test (MET): A vertical facility for hot tests of cryogenic engines (up to 216 kN) and integrated stages.
o Thrust Chamber Test (TCT): Primarily used for pressure-fed developmental tests and high-altitude (HAT) flight acceptance of CE20 engines.
o Subscale Engine Test (SET): The pioneering cryogenic facility at IPRC, used for testing steering engines and turbopump sub-systems.
o Redundant and Upcoming Infrastructure: To increase throughput, IPRC has commissioned the Cryogenic Turbo-Pump Test (CTPT) facility and is realizing the Integrated Cryo Engine & Stage Test (ICET) facility, a mammoth 42-metre tall structure
• Semi-Cryogenic Integrated Engine & Stage Test (SIET): A state-of-the-art facility featuring twin test bays for the development of high-thrust 2000 kN semi-cryogenic engines using Isrosene and Liquid Oxygen.
• High Altitude Test (HAT) Facilities: Specialized vacuum environments (LUS-TF, STTF, and NLTF) used to qualify upper-stage engines like the PS4 and spacecraft thrusters like the Liquid Apogee Motor (LAM).
III. Specialized Engineering and Support Infrastructure
IPRC’s mission success is underpinned by advanced laboratories and production plants.
• Propellant Production and Management: The complex operates a Liquid Hydrogen Production Plant with a capacity of hundreds of tonnes, ensuring a sustainable supply of LH2, LOX, and LIN for the national space programme.
• Non-Destructive Testing (NDT): A 6 MeV Linear Accelerator (LINAC) facility enables high-energy X-ray imaging for the internal inspection of flight engines as a single unit.
• Metrology and Material Testing: These labs provide dimensional inspections with accuracies up to 15 nanometers and perform mechanical property evaluations in extreme environments, including low-temperature testing down to 20K.
• Structural Test Facility (STF):Dedicated to testing the structural integrity of pressurized hardware, such as propellant tanks, with a capacity to handle hardware up to 5 metres in diameter.
• Centralized De-mineralized Water Plant (CDMP): A facility producing high-purity water with a Zero-Liquid Discharge feature to comply with environmental norms.
IPRC’s mission success is underpinned by advanced laboratories and production plants.
• Propellant Production and Management: The complex operates a Liquid Hydrogen Production Plant with a capacity of hundreds of tonnes, ensuring a sustainable supply of LH2, LOX, and LIN for the national space programme.
• Non-Destructive Testing (NDT): A 6 MeV Linear Accelerator (LINAC) facility enables high-energy X-ray imaging for the internal inspection of flight engines as a single unit.
• Metrology and Material Testing: These labs provide dimensional inspections with accuracies up to 15 nanometers and perform mechanical property evaluations in extreme environments, including low-temperature testing down to 20K.
• Structural Test Facility (STF):Dedicated to testing the structural integrity of pressurized hardware, such as propellant tanks, with a capacity to handle hardware up to 5 metres in diameter.
• Centralized De-mineralized Water Plant (CDMP): A facility producing high-purity water with a Zero-Liquid Discharge feature to comply with environmental norms.
IPRC Achievements
The ISRO Propulsion Complex (IPRC) has been the cornerstone of India’s space achievements, transforming complex propulsion concepts into the reliable power required for celestial exploration. Since its inception, the complex has reached critical milestones that have defined the success of the PSLV, GSLV, and LVM3 launch vehicle programmes.
I. Historical Milestones: A Legacy of Propulsion Excellence
The journey of the ISRO Propulsion Complex (IPRC) is a testament to India's pursuit of self-reliance in liquid, cryogenic, and semi-cryogenic rocket technology. From its humble beginnings in the early 1980s to its current status as a global leader, the complex has reached several critical technical landmarks:
• 1982: Establishment of the centre at Mahendragiri to support the growing needs of the Indian space programme.
• 1984: Realization of the Multidisciplinary Test Facility with remote control and monitoring instrumentation.
• December 28, 1985: A major breakthrough with the first successful hot test firing in the history of Mahendragiri, conducted with the Gas Generator.
• March 26, 1987: The "baby-step" towards cryogenic mastery with the first single-element injector test conducted using Gaseous Hydrogen and Liquid Oxygen at the SET facility.
• May 6, 1987: The first test on the Turbo-Pump of the Vikas Engine was successfully performed.
• October 31, 1987: The realization of total instrumentation culminated in the first VIKAS engine ignition test for a duration of 20 seconds at the Principal Test Stand (PTS).
• 1992: Marking a new era in simulated space environment testing, the first firing of the Liquid Apogee Motor (LAM) engine was carried out at the High Altitude Test (HAT) facility.
• June 27, 1993: The first cryogenic thrust chamber test was conducted at the SET facility.
• 1994: Inception of the Main Engine & Stage Test (MET) facility for cryogenic systems.
• November 15, 1995: Successful completion of the second cryogenic thrust chamber test at SET, applying lessons learned from earlier trials.
• 1996: A revolution in data acquisition occurred with the adoption of PXI DAS, leading the way for hardware uniformity across the complex. The TPT and SST facilities were also established to support the CUS programme.
• February 16, 2000: A historic moment for indigenous technology as the first indigenous cryogenic engine (A0) was integrated and tested at the MET facility.
• 2005: Establishment of dedicated facilities for the CUS/C25 programme.
• Late 2008: Technological progress in visualization led to the development of the first video wall for state-of-the-art online test monitoring.
• September 8, 2010: Achieved a momentous milestone with the successful testing of the L110 development stage.
• 2010: Establishment of the Spacecraft Thruster Test Facility (STTF) for the development and qualification of AOCS thrusters.
• Early 2010s: Migration to high-speed fiber and internet-based networks for transferring bulk test data from stands to the control room.
• 2013: Commissioning of the Cryogenic Sub-system Test Facility (CST) for testing with actual cryogenic fluids.
• February 1, 2014: The centre was officially elevated and renamed as the ISRO Propulsion Complex (IPRC).
• 2018: Initiation of the "Make in India" project for the indigenous development of Hot/Standby PLCs with very low cycle time in collaboration with ECIL.
• December 20, 2020: Inception of the Structural Test Facility (STF) to meet demands for pressurized hardware testing.
• December 31, 2021: A rare technical feat involving the ground recreation of a flight anomaly for the Fuel Booster Turbo-Pump.
• May 10, 2023: The first Power Head Test Article (PHTA) test was successfully conducted at the SIET facility.
• February 27, 2024: The Semi-cryo Integrated Engine Test (SIET) facility was formally dedicated to the nation by the Honourable Prime Minister.
• December 2024: Commissioning of the Centralised De-mineralised Water Plant (CDMP) featuring Zero-Liquid Discharge (ZLD) technology.
• 2025: Successful execution of the PHTA-R series of hot tests and commissioning of the Cryogenic Turbo-Pump Test Facility (CTPT)
.• July 2025: Commissioning of the New LAM Test Facility (NLTF) for HAT mode testing.
• June 2026 (Planned): Expected completion and commissioning of the Integrated Cryo Engine & Stage Test (ICET) facility, featuring a 42-metre tall twin-bay structure.
The journey of the ISRO Propulsion Complex (IPRC) is a testament to India's pursuit of self-reliance in liquid, cryogenic, and semi-cryogenic rocket technology. From its humble beginnings in the early 1980s to its current status as a global leader, the complex has reached several critical technical landmarks:
• 1982: Establishment of the centre at Mahendragiri to support the growing needs of the Indian space programme.
• 1984: Realization of the Multidisciplinary Test Facility with remote control and monitoring instrumentation.
• December 28, 1985: A major breakthrough with the first successful hot test firing in the history of Mahendragiri, conducted with the Gas Generator.
• March 26, 1987: The "baby-step" towards cryogenic mastery with the first single-element injector test conducted using Gaseous Hydrogen and Liquid Oxygen at the SET facility.
• May 6, 1987: The first test on the Turbo-Pump of the Vikas Engine was successfully performed.
• October 31, 1987: The realization of total instrumentation culminated in the first VIKAS engine ignition test for a duration of 20 seconds at the Principal Test Stand (PTS).
• 1992: Marking a new era in simulated space environment testing, the first firing of the Liquid Apogee Motor (LAM) engine was carried out at the High Altitude Test (HAT) facility.
• June 27, 1993: The first cryogenic thrust chamber test was conducted at the SET facility.
• 1994: Inception of the Main Engine & Stage Test (MET) facility for cryogenic systems.
• November 15, 1995: Successful completion of the second cryogenic thrust chamber test at SET, applying lessons learned from earlier trials.
• 1996: A revolution in data acquisition occurred with the adoption of PXI DAS, leading the way for hardware uniformity across the complex. The TPT and SST facilities were also established to support the CUS programme.
• February 16, 2000: A historic moment for indigenous technology as the first indigenous cryogenic engine (A0) was integrated and tested at the MET facility.
• 2005: Establishment of dedicated facilities for the CUS/C25 programme.
• Late 2008: Technological progress in visualization led to the development of the first video wall for state-of-the-art online test monitoring.
• September 8, 2010: Achieved a momentous milestone with the successful testing of the L110 development stage.
• 2010: Establishment of the Spacecraft Thruster Test Facility (STTF) for the development and qualification of AOCS thrusters.
• Early 2010s: Migration to high-speed fiber and internet-based networks for transferring bulk test data from stands to the control room.
• 2013: Commissioning of the Cryogenic Sub-system Test Facility (CST) for testing with actual cryogenic fluids.
• February 1, 2014: The centre was officially elevated and renamed as the ISRO Propulsion Complex (IPRC).
• 2018: Initiation of the "Make in India" project for the indigenous development of Hot/Standby PLCs with very low cycle time in collaboration with ECIL.
• December 20, 2020: Inception of the Structural Test Facility (STF) to meet demands for pressurized hardware testing.
• December 31, 2021: A rare technical feat involving the ground recreation of a flight anomaly for the Fuel Booster Turbo-Pump.
• May 10, 2023: The first Power Head Test Article (PHTA) test was successfully conducted at the SIET facility.
• February 27, 2024: The Semi-cryo Integrated Engine Test (SIET) facility was formally dedicated to the nation by the Honourable Prime Minister.
• December 2024: Commissioning of the Centralised De-mineralised Water Plant (CDMP) featuring Zero-Liquid Discharge (ZLD) technology.
• 2025: Successful execution of the PHTA-R series of hot tests and commissioning of the Cryogenic Turbo-Pump Test Facility (CTPT)
.• July 2025: Commissioning of the New LAM Test Facility (NLTF) for HAT mode testing.
• June 2026 (Planned): Expected completion and commissioning of the Integrated Cryo Engine & Stage Test (ICET) facility, featuring a 42-metre tall twin-bay structure.
II.Strategic Contributions to National Missions
IPRC has played an exceptional role in propelling India’s most prestigious space missions:
• Chandrayaan-3: Successfully performed critical propulsion system testing on the Lunar module, directly contributing to the vehicle's successful journey to the Moon.
• Gaganyaan Programme: Undergoing meticulous planning for India’s first human spaceflight, IPRC has already achieved major milestones, including the qualification of the L110 liquid engines and the high-thrust CE20 cryogenic engines.
• Mars Orbiter Mission (MOM): Conducted pivotal ground simulation tests and demonstrated the restart capability of the LAM engine after its long hibernation in deep space.
IPRC has played an exceptional role in propelling India’s most prestigious space missions:
• Chandrayaan-3: Successfully performed critical propulsion system testing on the Lunar module, directly contributing to the vehicle's successful journey to the Moon.
• Gaganyaan Programme: Undergoing meticulous planning for India’s first human spaceflight, IPRC has already achieved major milestones, including the qualification of the L110 liquid engines and the high-thrust CE20 cryogenic engines.
• Mars Orbiter Mission (MOM): Conducted pivotal ground simulation tests and demonstrated the restart capability of the LAM engine after its long hibernation in deep space.
III. Technological Breakthroughs and Innovation
IPRC continues to push the boundaries of materials science and engine design:
• Bootstrap Mode Milestone: Achieved a first-of-its-kind milestone by demonstrating the bootstrap mode start of the CE20 engine, a critical restart capability for advanced flight profiles.
• Additive Manufacturing (3D Printing): Successfully tested the first additive manufactured (AM) engine for a duration of 665 seconds, demonstrating a promising, cost-effective alternative for future propulsion hardware.
• Advanced Nozzle Technology: Completed successful long-duration testing of the PS4 engine utilizing advanced Carbon-Carbon and Stellite nozzle materials, designed to survive extreme thermal loads.
• Nozzle Protection System (NPS): Developed and qualified an indigenous NPS that allows cryogenic engines to be tested under ambient sea-level conditions, significantly optimizing test resources by eliminating the constant need for high-altitude facilities.
IPRC continues to push the boundaries of materials science and engine design:
• Bootstrap Mode Milestone: Achieved a first-of-its-kind milestone by demonstrating the bootstrap mode start of the CE20 engine, a critical restart capability for advanced flight profiles.
• Additive Manufacturing (3D Printing): Successfully tested the first additive manufactured (AM) engine for a duration of 665 seconds, demonstrating a promising, cost-effective alternative for future propulsion hardware.
• Advanced Nozzle Technology: Completed successful long-duration testing of the PS4 engine utilizing advanced Carbon-Carbon and Stellite nozzle materials, designed to survive extreme thermal loads.
• Nozzle Protection System (NPS): Developed and qualified an indigenous NPS that allows cryogenic engines to be tested under ambient sea-level conditions, significantly optimizing test resources by eliminating the constant need for high-altitude facilities.
IV. Strategic Infrastructure and Indigenisation
Our commitment to the "Make in India" policy has led to significant advancements in self-reliance:
• Indigenous Automation: Developed a high-speed Hot/Standby in collaboration with ECIL.
• Semi-Cryogenic Leadership: The Semi-Cryo Integrated Engine Test Facility (SIET) was dedicated to the nation in 2024, representing the pinnacle of IPRC’s mastery in high-thrust (2000 kN) engine testing.
• Sustainable Infrastructure: Established the Centralised De-mineralised Water Plant (CDMP), which utilizes a Zero-Liquid Discharge (ZLD)feature to meet stringent environmental standards while supporting all complex-wide test activities.
Our commitment to the "Make in India" policy has led to significant advancements in self-reliance:
• Indigenous Automation: Developed a high-speed Hot/Standby in collaboration with ECIL.
• Semi-Cryogenic Leadership: The Semi-Cryo Integrated Engine Test Facility (SIET) was dedicated to the nation in 2024, representing the pinnacle of IPRC’s mastery in high-thrust (2000 kN) engine testing.
• Sustainable Infrastructure: Established the Centralised De-mineralised Water Plant (CDMP), which utilizes a Zero-Liquid Discharge (ZLD)feature to meet stringent environmental standards while supporting all complex-wide test activities.
V. Operational Excellence and Quality
IPRC maintains an unmatched track record of reliability:
• Human Safety: IPRC’s faster abort reaction times have repeatedly safeguarded multi-crore engine hardware during developmental trials.
• Transducer Leadership: Annually calibrates and supplies nearly 2,000 high-precision transducers for flight stages across the PSLV, GSLV, and LVM3 programmes.
IPRC maintains an unmatched track record of reliability:
• Human Safety: IPRC’s faster abort reaction times have repeatedly safeguarded multi-crore engine hardware during developmental trials.
• Transducer Leadership: Annually calibrates and supplies nearly 2,000 high-precision transducers for flight stages across the PSLV, GSLV, and LVM3 programmes.
