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Next Generation Launch Vehicle
Next Generation Launch Vehicle
Next Generation Launch Vehicle
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Next Generation Launch Vehicle
NGLV, NGLV-H and NGLV-SH
FunctionMedium to Heavy-lift launch vehicle
ManufacturerISRO
Country of originIndia
Size
Height93 m (305 ft)[1]
Width6.5 m (21 ft)[2]
Mass600 t (590 long tons; 660 short tons) to 1,094 t (1,077 long tons; 1,206 short tons)
Booster stage – S200 Boosters (NGLV-H)
Height25 m (82 ft)[3]
Diameter3.2 m (10 ft)[4]
Empty mass31,000 kg (68,000 lb) each[5]
Gross mass236,000 kg (520,000 lb) each[5]
Propellant mass205,000 kg (452,000 lb) each[5]
Powered bySolid S200
Maximum thrust5,151 kN (525.3 tf)[6][7]
Specific impulse274.5 seconds (2.692 km/s) (vacuum)[5]
Burn time128 s[5]
PropellantHTPB / AP[5]
First stage – LM470 Core (NGLV/NGLV-H)
Diameter6.5 m (21 ft)
Propellant mass470 t (1,040,000 lb)
Powered by9 LME-110
PropellantLOX / CH4
Second stage – LM120 (NGLV/NGLV-H)
Diameter6.5 m (21 ft)
Propellant mass120 t (260,000 lb)
Powered by2 LME-110
PropellantLOX / CH4
Third stage – C32 (NGLV/NGLV-H)
Diameter6.5 m (21 ft)[5]
Propellant mass32 t (71,000 lb)[5]
Powered by1 CE-20
Maximum thrust216 kN (22.0 tf)[5]
Specific impulse443 seconds (4.34 km/s)
PropellantLOX / LH2
Stages3
Capacity
Payload to LEO
MassNGLV: 14 t (31,000 lb) (Reused)
20 t (44,000 lb) (Expended)
NGLV-H: 30 t (66,000 lb)[8]
Payload to GTO
MassNGLV: 5 t (11,000 lb) (Reused)
9 t (20,000 lb) (Expended)
NGLV-H: 12 t (26,000 lb)
Payload to TLI
MassNGLV: 7 t (15,000 lb)
NGLV-H: 10 t (22,000 lb)[citation needed]
Associated rockets
Comparable
Launch history
StatusUnder development
Launch sitesSDSC TLP
First flight2031 (planned)
Carries passengers or cargo[9]
[edit on Wikidata]

The Next Generation Launch Vehicle (NGLV) is a family of three-stage partially reusable medium to super heavy-lift launch vehicle, currently under development by ISRO. The family of these vehicles are designed to replace currently operational systems like the PSLV and GSLV.[10] Previously referred to as Unified Launch Vehicle (ULV),[11] the project is now being called as Project Soorya.[12]

This family of three launchers were previously being designed for replacing the different core propulsion modules of PSLV, GSLV, and LVM3 respectively with a common semi-cryogenic engine and hence it was named as ULV.[13] The initial proposals were planned to be expendable. But the new (Oct 2022) proposals under the name of NGLV suggests launchers having partial reusability.[14]

S. Sivakumar is the program director for ISRO's Space Transportation System and the projector director for NGLV at the Vikram Sarabhai Space Centre (VSSC).[15][16] The development of the NGLV is projected to be 8 years from December 2024.[17]

In an interview, the former Chairman of ISRO S. Somanath stated that after the integration of the NGLV, all other launch vehicles will be retired, except the LVM3 and the SSLV.

History

[edit]

Development

[edit]

The launch system has been in development since 2010s and has gone through various design changes over time. As ISRO's launch vehicles were ageing, the need for a new generation of launchers with interchangeable modular parts was realised. There have been several design changes since the first proposal.

Initial proposals

[edit]

More than a decade after starting the Cryogenic Upper Stage Project in 1994,[18] ISRO began developing a new semi-cryogenic engine that would be used on its next generation of vehicles of Unified Launch Vehicle (now NGLV), Reusable Launch Vehicle (RLV) and a heavy-lift launcher for future inter-planetary missions. On 22 December 2008, the government approved the development of semi-cryogenic engine technology at an estimated cost of ₹1,798 crore (US$213 million), with a foreign exchange component of ₹588 crore (US$70 million), for the completion of the project by 2014, the engine was then named SE-2000 (now called the SE-2000).[19]

In May 2013, the configurations of the launchers were revealed for the first time. They had a common core and upper stage, with four different booster sizes.[20] The core, known as the SC160 (Semi-Cryogenic stage with 160 tonnes of propellant, in the ISRO nomenclature), would have 160,000 kg (350,000 lb) of Kerosene / LOX propellant and be powered by a single SCE-200 (now called the SE-2000) engine. The upper stage, known as the C30 (Cryogenic stage with 30 tonnes of propellant) would have 30,000 kg (66,000 lb) of LH2 / LOX propellant and be powered by a single CE-20 engine.[21][22]

The four booster options were:

  • 6 × S-13, slightly larger than the S-12 on PSLV, to burn longer;
  • 2 × S-60, which appears to be a new solid motor development;
  • 2 × S-139, which is the first stage of PSLV and GSLV Mk I/II;
  • 2 × S-200, like on the LVM3.
ULVs' initial proposals with LVM3 for comparison.
Heavy-lift variant
[edit]

A potential heavy-lift variant (HLV) of the ULV, in theory was capable of placing up to 10 ton class of spacecraft into Geosynchronous Transfer Orbit. It was planned to include:[23]

  • A larger dual S-250 solid strap-on boosters as compared to the S-200 boosters used in LVM3;
  • A L-400 semi-cryogenic core stage, with 400 tonnes of propellant, using a cluster of five SCE-200 engines;
  • A L-27 cryogenic third stage, with 27 tonnes of propellant, using CE-20 engine;
Super-heavy-lift variant
[edit]

A super-heavy-lift variant, was also among the proposals. With multiple SCE-200 engines and side boosters, this variant would have been the most powerful rocket that ISRO had ever developed.[22]

Partial reuse, for NGLV

[edit]

In Oct 2022 it was suggested that the boosters and first stage of NGLV would be reusable.[14]

Renaming and cabinet approval

[edit]

S.Somanath, speaking to NDTV on 29 June 2024, unveiled a proposal to officially rename the NGLV as "Soorya". It will be used to help complete the Bharatiya Antariksh Station (BAS) by 2035 and send an Indian to the moon by 2040.[24]

Under the direction of Prime Minister Narendra Modi, the Union Cabinet approved the development of the Next-Generation Launch Vehicle on September 18, 2024. This move bolsters India's ambition to establish and run the BAS and accomplish a crewed lunar landing by 2040.[25][26] The NGLV has been approved for ₹8,240 crore (US$970 million) in total. It will be implemented over 96 months (8 years) and comprises financing for program administration, facility establishment, and three developmental flights (D1, D2 & D3). It is anticipated that the private space industry would be crucial to the manufacturing and development process, easing the transfer from development to operational status.[27][28] The development of the NGLV is projected to take another 8 years from December 2024.[17]

Design

[edit]

NGLV will have a simple, robust architecture that enables bulk production and modularity in stages, subsystems, and systems for quick turnaround times.[29] It's possible that the NGLV will be a three-stage rocket that runs on green fuel mixes, such as liquid oxygen and kerosene or methane and liquid oxygen for the SCE-200 engine, which runs on an oxidizer-rich closed combustion engine cycle. The first launch is slated for 2034–2035.[30]

According to ISRO Chairman S. Somanath, the new rocket has a load capacity of between 20 and 1,215 tonnes.[31] Industry players will handle the production and launches from the outset, with ISRO contributing to the development process.[32]

ISRO is seeking to add vertical takeoff, vertical landing (VTVL) capability in NGLV first stage and booster stage. Vikram Sarabhai Space Centre is developing advanced navigation system, as well as steerable grid fins, deployable landing legs, and advanced avionics.[15][16] In order to save costs, the conceptualization, development and testing of new technologies for NGLV will be done on a small-scale vehicle (possibly ADMIRE test vehicle).[33][34] It will be possible to recover NGLV both on land and in the sea, according to S. Somanath. The recovery landing test will initially take place on land. Later on, a sea test of a similar nature will be conducted.[35]

During the assembly process, the NGLV will be horizontally erected at the launch pad. Several changes are being accommodated in the design of the third launch pad at SDSC for the rocket.[36]

Modifications and partial reusability

[edit]
SCE-200 (also referred as Semi-Cryogenic Engine-200) developed by Liquid Propulsion Systems Centre for LVM3 and Next Generation Launch Vehicle.

The development of the SCE-200 engine was completed in 2017 and the tests were contracted to a Ukrainian manufacturer Yuzhmash. In September 2021, in a virtual event being conducted by ISRO, the presentation mentioned a fleet configuration of a family of five rockets capable of lifting from 4.9 tonnes to 16 tonnes to geostationary transfer orbit (GTO). The presentation mentioned the ongoing development of a new semi-cryogenic stage namely SC120 and an upgraded cryogenic stage namely C32. The configurations displayed more powerful engine stages; SC-400 semi-cryogenic stage, C27 cryogenic stage, and S-250 solid rocket boosters.[37]

In June 2023, ISRO revealed that the team working on the NGLV programme had already submitted a preliminary report on the rocket's details, manufacturing process, and approach toward development. The rocket is planned to be partially reusable along with its boosters. The development was expected to take another five to ten years.[38]

Following several months of preliminary planning and design and architectural refinement, ISRO has established a project team to begin construction of the NGLV. The third launch pad at Sriharikota will be required because the NGLV project, internally named "Soorya," will differ from the current class of rockets in configuration. This was confirmed by ISRO chairman S. Somanath in an exclusive interview with The Times of India. The development of NGLV will involve teams with backgrounds in LVM3, GSLV, PSLV, and SSLV.[39]

Propulsion technology

[edit]
Hot test of SCE-200 Power Head Test Article (PHTA) in intermediate configuration at ISRO Propulsion Complex.

With the aim of sending humans to the moon by 2040, ISRO has begun working on future technology development initiatives. It is expected that thirty tons of payload will be transported using rockets. A Memorandum of Understanding (MoU) was signed on September 4, 2024, by the Raja Ramanna Centre for Advanced Technology (RRCAT) and the LPSC to jointly develop propulsion technology capable of lifting up to 30 tonnes and conveniently transporting bigger payloads to space and the moon. Eighteen to twenty-four months is the maximum time allotted for technology development.[40][41]

The launch vehicle's engine will use methane and liquid oxygen for propulsion. For engine development, RRCAT will make use of Laser Additive Manufacturing (LAM). According to Dr. V. Narayanan, the director of LPSC, Soorya will require a minimum of 25 rocket engines; therefore, the current annual capacity of producing 2-3 engines will be upgraded. The physical construction of the engine will take eight years. Initially, the engine will be utilized to send cargo into orbit. Once the engine passes human-rating certification, Indian astronauts would be able to travel to the moon.[40][41]

ISRO is working on bringing capabilities for multiple restarts. It will aid in booster stage recovery as well as upper stage mission flexibility. ISRO is developing a spark torch igniter for the future LOX-Methane stages that will have higher ignition reliability and also cleaner combustion products.[42] A sub-scale thrust chamber model was developed and tested by LPSC and IPRC in late-January 2026 to evalute the design for a LOX-Methane engine for induction in the NGLV Programme under the LMSE HT-03 development programme.[43]

List of launches

[edit]
Flight No. Date / time (UTC) Rocket,
Configuration 		Launch site Payload Payload mass Orbit User Launch
Outcome
D1 2031 (TBD) NGLV Third India TBA LEO ISRO Planned
Maiden flight of ISRO's Next Generation Launch Vehicle (NGLV).[30]
D2 2032 (TBD) NGLV Third India TBA ISRO Planned
[30]
D3 2032 (TBD) NGLV Third India TBA ISRO Planned
The NGLV First Stage Booster is planned to be recovered in this Mission.[30]
2033-34 (TBD) NGLV-H Third India TBA ISRO Planned
Maiden flight of ISRO's Next Generation Launch Vehicle-Heavy (NGLV-H), A Variant of NGLV.[30]
2033-34 (TBD) LMLV Third India TBA ISRO Planned
Maiden flight of ISRO's Lunar Module Launch Vehicle (LMLV).[30]
2033-34 (TBD) LMLV Third India Chandrayaan-6 ISRO Planned
Landing of Same lander as the Crewed Lunar Descent stage.[44]
2033-34 (TBD) LMLV Third India Chandrayaan-7 ISRO Planned
First of Two Uncrewed End-to-End Lunar Human Landing Demonstration.[45]
2036-37 (TBD) LMLV Third India Chandrayaan-8 ISRO Planned
Second of Two Uncrewed End-to-End Lunar Human Landing Demonstration.[46]
2038-39 (TBD) LMLV Third India Chandrayaan-H1 Crew Module ISRO Planned
Indian first crewed Lunar mission, will orbit the Moon and return.[47]
2040 (TBD) LMLV Third India Chandrayaan-H2 Earth Departure Stage LEO to Selenocentric ISRO Planned
First of two launches for Chandrayaan-H2 Mission, First Indian Crewed landing on the surface of the Moon.[30]
2040 (TBD) LMLV Third India Chandrayaan-H2 Crew Module & Lander Module LEO to Selenocentric ISRO Planned
Second of two launches for Chandrayaan-H2 Mission, First Indian Crewed landing on the surface of the Moon.[30]

Potential uses and problems

[edit]

As per a presentation done by S. Somanath at a conference in October 2022, the NGLV might offer launch costs of approximately $1900 per kg of payload in the reusable form and nearly $3000 per kg in the expendable format. The vehicle will also help in meeting India's need of setting up its space station by 2035. Other potential use cases will be in the areas of launching communication satellites, deep space missions, future human spaceflight, and cargo missions.[48][49]

Somanath also stated that as of now, the demand for such a high end rockets were low as there were very few customers who are required in such high end rockets and rockets are already available in the global market which creates a heavy competition for ISRO with other space agencies and private organisations if such high end rockets were created.[50]

For the 2040 crewed lunar landing mission, ISRO will rely on multiple launches and docking technology rather than building a big rocket.[51]

LMLV

[edit]
Lunar Module Launch Vehicle
Illustration of LMLV
FunctionSuper heavy-lift launch vehicle
ManufacturerISRO
Country of originIndia
Size
Height116 m (381 ft)[52]
Width5 m (16 ft)
Mass2,614 t (2,573 long tons; 2,881 short tons)
Boosters stage – LM650 Booster
Diameter5.0 m (16.4 ft)
Propellant mass650 t (1,430,000 lb)
Powered by9 LME-110
PropellantLOX / CH4
First stage – LM650 Core
Diameter5.0 m (16.4 ft)
Propellant mass650 t (1,430,000 lb)
Powered by9 LME-110
PropellantLOX / CH4
Second stage – LM200
Diameter5.0 m (16.4 ft)
Propellant mass200 t (440,000 lb)
Powered by2 LME-110
PropellantLOX / CH4
Third stage – C70
Diameter5.0 m (16.4 ft)[5]
Propellant mass70 t (150,000 lb)[5]
Powered by1 CE-20
Maximum thrust216 kN (22.0 tf)[5]
Specific impulse443 seconds (4.34 km/s)
PropellantLOX / LH2
Stages3
Capacity
Payload to LEO
Mass75 t (165,000 lb)[53]
Payload to GTO
Mass24 t (53,000 lb)[citation needed]
Payload to TLI
Mass26 t (57,000 lb)[citation needed]
Associated rockets
Comparable
Launch history
StatusUnder development
Launch sitesSDSC TLP
First flight2031 (planned)
Carries passengers or cargo[54]
[edit on Wikidata]

The Lunar Module Launch Vehicle (LMLV) is a three-stage partially reusable super heavy-lift launch vehicle, currently under development by ISRO. LMLV is planned to be used in Indian Lunar Human Spaceflight Mission.[55][56]

See also

[edit]

References

[edit]
Revisions and contributorsEdit on WikipediaRead on Wikipedia

Next Generation Launch Vehicle

View on Grokipedia
from Grokipedia
The Next Generation Launch Vehicle (NGLV) is a partially reusable, three-stage under development by the Indian Space Research Organisation () to enable cost-effective access to space for advanced missions. It features a reusable booster stage powered by liquid oxygen-methane engines and two expendable upper stages, designed to deliver a maximum of 30 metric tonnes to (LEO). With three times the capacity of ISRO's current at 1.5 times the operational cost, the NGLV incorporates modular green propulsion systems to support , satellite constellations, and deep . Approved by the Union Cabinet in September 2024 with a total budget of ₹8,240 , the NGLV project spans 96 months and includes three developmental flights to validate its performance. The initiative emphasizes maximal participation from Indian industry, including investments in manufacturing capabilities, to align with national goals . It is positioned to succeed ISRO's current Mark-3 () and thereby enhance India's launch capacity from up to 10 tonnes to LEO and 4 tonnes to (GTO). The NGLV's development focuses on key objectives like supporting the Bharatiya Antariksh Station and enabling an Indian crewed lunar by 2040, marking a significant evolution in ISRO's launch infrastructure. The (LPSC) leads the propulsion efforts, developing components such as the LME1100 LOX-methane engine, the LM450 reusable first stage with nine such engines, the LM120 second stage with twin engines, and the C32 cryogenic third stage. Recent milestones include ignition trials for spark torch igniters to enable multiple restarts of vehicle stages, underscoring the project's progress toward reliable reusability.

Development History

Initial Concepts

In the post-2010 period, the outlined a strategic vision for advancing its launch capabilities to support high-priority objectives, including missions such as crewed lunar landings and the deployment of large-scale satellite constellations for enhanced communication and . This roadmap, detailed in official sector overviews, prioritized the evolution toward heavier-lift and reusable systems to overcome the constraints of existing vehicles like the Mark III (GSLV Mk III), which limited payloads to approximately 4 tonnes in Geosynchronous Transfer Orbit (GTO). Initial proposals for what would become the Next Generation Launch Vehicle (NGLV) emerged between and 2018, focusing on a partially reusable significantly surpassing the GSLV Mk III's limitations and enabling more ambitious deep-space and orbital missions. These concepts drew from ongoing reusable technology demonstrations, such as the Reusable Launch Vehicle Technology Demonstrator (RLV-TD) flight, which validated autonomous re-entry and landing mechanisms essential for in future operations. The proposed design emphasized to streamline production and adaptability across mission profiles. ISRO's Launch Vehicle Programme Office spearheaded key feasibility studies during this phase, including detailed cost-benefit analyses that evaluated the economic advantages of partial reusability, such as booster recovery, against traditional expendable configurations. These reports highlighted potential cost reductions in launch costs through repeated use of first-stage elements, while addressing technical challenges like thermal protection and reliability. The project was initially designated as the "Next Generation Launch Vehicle" to clearly differentiate it from operational workhorses like the (PSLV) and , signaling a shift toward next-era capabilities in India's space portfolio. This naming reflected ISRO's intent to integrate lessons from the as a baseline for scalability.

Approval Process

The Union Cabinet approved the development of the Next Generation Launch Vehicle (NGLV) on September 18, 2024, allocating a of ₹8,240 crore to support the program's initiation and execution over an eight-year timeline. This decision, chaired by Prime Minister Narendra Modi, formalized governmental backing for ISRO's efforts to create a partially reusable heavy-lift capable of supporting future missions, including the Bharatiya Antariksh Station. The approval encompassed funding for design, prototyping, and three developmental flights (D1, D2, and D3), aimed at validating the vehicle's performance by approximately 2032. In early 2025, internal discussions within considered renaming the vehicle to Lunar Module Launch Vehicle (LMLV) to emphasize its role in lunar missions, particularly for variants optimized for to the Moon. This proposal briefly highlighted a focus on lunar-specific configurations, such as those without strap-on boosters for direct insertion, but was ultimately set aside in favor of retaining NGLV as the overarching family name to encompass broader applications, including payloads up to 30 tons. ISRO has explored international collaborations to accelerate development, particularly for reusability technologies like autonomous landing systems and , engaging with global partners for potential knowledge sharing and technology transfers. However, as of November 2025, no binding agreements have been finalized, with efforts prioritizing indigenous capabilities while maintaining openness to joint ventures that align with India's space policy. Key milestones include the 2024 greenlight, with initial component prototypes—such as semi-cryogenic engines—targeted for ground testing by 2028 to inform full vehicle integration.

Current Status

As of November 2025, the development of the Next Generation Launch Vehicle (NGLV) by the remains in the early conceptual and design phases, with active efforts focused on key technologies such as reusable stages and advanced propulsion systems. has issued expressions of interest for critical components, including the fabrication of tanks using , indicating progression toward development. Subscale testing of reusable components, including ignition trials for LOX-methane engines intended for the reusable booster stage, is being conducted at the in . The project received approval in September 2024 with a total allocated of ₹8,240 to cover development costs, three developmental flights, and necessary over an eight-year timeline. By mid-2025, initial expenditures have supported activities, though specific progress on budget utilization reflects the project's nascent stage, with foundational work on engines and materials ongoing. The NGLV is a cornerstone of India's broader space vision through 2040, designed to enable sustainable access to space and align with ambitious programs such as for demonstrations and the Chandrayaan lunar exploration series. It supports the establishment of the Bharatiya Antariksh Station by 2035 and facilitates crewed lunar missions by 2040, enhancing payload capacities for these initiatives beyond current launchers like the LVM3. Recent announcements from indicate that the maiden developmental flight of the NGLV is targeted for 2032, marking the completion of the initial development phase, with subsequent human-rating processes planned to certify it for lunar missions by 2035.

Vehicle Design

Configuration and Stages

The Next Generation Launch Vehicle (NGLV) employs a three-stage to achieve efficient orbital insertion. The first stage functions as the primary booster, generating the required for initial ascent through the dense lower atmosphere. The second stage is engineered for optimal performance in the of , bridging the transition from atmospheric flight to upper orbital phases. The third stage provides the fine control necessary for accurate payload deployment into target orbits, such as or geostationary transfer orbit (GTO). The overall vehicle measures approximately 90-100 meters in height and features a core diameter of 5-6 meters, enabling it to accommodate substantial loads while maintaining structural efficiency. This design supports modular variants tailored to mission requirements, with the base configuration capable of delivering ~30 tonnes to (LEO) or ~10 tonnes to GTO as of 2025. The first stage incorporates reusability elements to enable recovery after separation. Structural innovations in the NGLV emphasize weight reduction and durability through the use of advanced composites, scaled up from those applied in the launch vehicle for components like shrouds and equipment bays. These materials enhance structural integrity under extreme launch conditions while minimizing mass. Payload fairing options include a standard 5-meter for accommodating typical sizes, with expandable configurations up to 6 meters to support larger modules or deployable structures.

Reusability Elements

The Next Generation Launch Vehicle (NGLV) incorporates partial reusability to enhance cost efficiency, focusing primarily on the recovery and refurbishment of its first stage. This approach draws inspiration from established vertical takeoff and vertical landing (VTVL) technologies, adapted to Indian engineering standards by the Indian Space Research Organisation (ISRO). The first stage is designed for powered descent and landing, enabling either return to the launch site or downrange recovery, which supports multiple missions per booster while maintaining operational reliability. Key reusability elements include steerable grid fins for atmospheric reentry control and deployable landing legs for touchdown stability, integrated with advanced and systems developed by ISRO's (VSSC). These features allow the first stage to perform precise maneuvers during descent, similar to proven international designs but optimized for NGLV's LOX-methane engines and structural materials. Recovery options extend to sea landings, with ISRO planning infrastructure for both land-based and oceanic retrieval to accommodate varied mission profiles. In contrast, the second and third stages of the three-stage NGLV configuration remain expendable, prioritizing precision orbital insertion and payload deployment over recovery to ensure mission success rates. This hybrid design balances reusability benefits with the technical demands of upper-stage operations, where refurbishment could compromise accuracy. aims to demonstrate these elements through a series of development flights within an eight-year timeline, targeting operational reusability to achieve low-cost access to .

Propulsion Systems

The propulsion systems of the Next Generation Launch Vehicle (NGLV) are engineered to balance high requirements for initial ascent with for orbital insertion, incorporating advanced liquid technologies developed by the Indian Space Research Organisation (). These systems emphasize LOX-methane engines for the lower stages to support reusability, with a cryogenic upper stage, as of 2025. The selection of propellants and engine designs draws from 's ongoing advancements in liquid , focusing on throttleable engines for controlled descent and restart capabilities for precise deployment. The first stage (LM450) utilizes a cluster of nine LOX-methane (LCH4) engines (LME1100), each delivering approximately 1100 kN of . This configuration enables robust sea-level with a (Isp) of around 310-320 seconds, supporting reusability through deep throttling for landing maneuvers. The stage achieves a high , maximizing payload efficiency. The second stage (LM120) is powered by two LME1100 /LCH4 engines, providing vacuum thrust of ~2200 kN total. This setup offers an Isp exceeding 330 seconds for efficient velocity gains during mid-ascent, ensuring smooth transition to the upper stage. Its design supports reliable ignition and sustained burn for diverse mission profiles. The third stage (C32) features a restartable cryogenic upper stage powered by an uprated engine, operating on and (LH2) propellants with approximately 220 kN of thrust. Using ~32 tonnes of propellants (up from C25's 25 tonnes), this engine variant incorporates enhanced restart mechanisms tested in recent trials (as of 2025), allowing multiple ignitions for maneuvering. It prioritizes high Isp (around 450 seconds) in the environment to minimize fuel consumption during final adjustments, increasing capacity by ~25% over predecessors. Overall, these propulsion elements integrate with the vehicle's staging for seamless separation, with the first stage's engine cluster providing the primary thrust vector control. The reflects ISRO's emphasis on indigenous development, drawing from human-rated qualifications of similar engines to ensure reliability for heavy-lift operations.

Performance Specifications

Payload Capabilities

The Next Generation Launch Vehicle (NGLV) demonstrates enhanced delivery capabilities compared to predecessor systems, enabling a broader range of missions including satellite constellations and interplanetary probes. In its baseline configuration, the NGLV can deliver 10 tonnes to Geosynchronous Transfer Orbit (GTO), providing sufficient lift for heavy communication that current vehicles like the struggle to accommodate in single launches. For (LEO), the vehicle achieves up to 30 tonnes as of 2025. Performance is influenced by operational modes, particularly reusability of the first stage, which supports cost-effective access while maintaining high lift efficiency, with the systems contributing to overall optimization. The vehicle's fairing and upper stage design further mitigate environmental factors like atmospheric drag and thermal loads, preserving integrity across varying launch windows. To maximize utility for constellation deployments, the NGLV incorporates a multi-payload adaptor system capable of accommodating 4-6 satellites per launch, ideal for scaling systems like NavIC expansions with multiple regional navigation spacecraft. This configuration leverages standardized interfaces for rapid integration, reducing per-satellite costs and enabling frequent rideshare opportunities. The NGLV is designed to support missions, integrating features from the program to ensure reliable performance.

Operational Features

The Next Generation Launch Vehicle (NGLV) is engineered to support flexible trajectory profiles tailored to mission requirements, including direct ascent paths to (GTO) for efficient satellite deployment and multi-burn sequences for deep space transfers such as lunar missions. These options leverage the vehicle's three-stage architecture and reusable first stage to optimize fuel efficiency and payload delivery, enabling to address a range of orbital insertion needs from to beyond. Guidance and navigation for the NGLV incorporate advanced inertial measurement units (IMUs) based on ring laser gyroscopes (RLGs), providing high-precision attitude and data during ascent. These systems are supplemented by GPS-aided navigation to achieve accurate orbital insertion, with ISRO's indigenous RLG technology ensuring robust performance across launch vehicles for dynamic environments. The integration of redundant sensors enhances , maintaining trajectory fidelity essential for complex missions. Safety and reliability are prioritized through redundant avionics architectures, targeting high mission success rates comparable to ISRO's established vehicles like the LVM3, which have demonstrated over 95% reliability in operational flights. This redundancy includes duplicated flight control computers and sensor arrays to mitigate single-point failures, supporting the NGLV's role in human-rated and critical payloads. Launches from Sriharikota necessitate adaptations to tropical environmental conditions, including wind shear compensation algorithms in the flight control system to counteract atmospheric disturbances during liftoff. These features account for regional constraints such as high humidity and seasonal cyclones, ensuring stable ascent profiles through real-time thrust vectoring and aerodynamic adjustments.

Planned Operations

Launch Schedule

The of the Next Generation Launch Vehicle (NGLV) is targeted for 2032 as an uncrewed demonstration mission from the , with a primary focus on validating first-stage recovery for reusability. In January 2025, the Union Cabinet approved the establishment of a Third Launch Pad at the to support NGLV and other advanced launch vehicles. This initial test will be the first of three planned development flights (D1, D2, and D3) to complete the vehicle's qualification within the program's 96-month development phase, approved in September 2024. Subsequent operational launches are projected to begin in the mid-2030s, initially supporting deployments for communication and constellations, including missions for the series to . From 2036 onward, the NGLV will enable human-rated missions, contributing to India's crewed lunar landing ambitions by 2040 through multiple launches involving in-orbit assembly and docking. The launches will be facilitated by extensive partnerships with Indian private industry to build manufacturing capacity and support commercial satellite operations.

Mission Applications

The Next Generation Launch Vehicle (NGLV) is poised to significantly enhance India's commercial space sector by enabling the launch of heavier communication satellites into (GTO), particularly for the Indian National Satellite (INSAT) system, which supports , , and applications. With a capacity approximately three times that of the current , the NGLV will allow ISRO's commercial arm, (NSIL), to offer competitive services for multi-tonne (GEO) missions, positioning India as a viable alternative to international providers. In the realm of scientific exploration, the NGLV will underpin ambitious interplanetary endeavors, including the Chandrayaan-4 mission for lunar sample return and prospective Mars lander operations to conduct surface experiments. Its heavy-lift capabilities, including substantial performance, will facilitate these deep-space missions by delivering complex spacecraft and instruments beyond , building on ISRO's successes like Chandrayaan-3. Additionally, the vehicle is set to support the for atmospheric and surface studies, expanding India's portfolio. For , the NGLV represents a cornerstone of India's crewed ambitions, providing the heavy-lift capacity required to assemble and resupply the Bharatiya Antariksh Station (BAS) in by 2035, accommodating modules and logistics for 3-6 astronauts. It will also enable crewed lunar missions, targeting an Indian landing by 2040 as part of a broader roadmap that includes orbital demonstrations and habitat precursors. These applications leverage the NGLV's human-rated design for safe, reliable transport of personnel and equipment.

Challenges and Future Prospects

Technical Hurdles

One of the primary technical hurdles in developing the Next Generation Launch Vehicle (NGLV) is achieving reliable reusability, particularly for the booster stage intended for multiple missions. The reusable elements must withstand the intense thermal loads during atmospheric reentry, where temperatures exceed 1600°C, necessitating advanced protection systems (TPS) capable of repeated use without significant degradation. ISRO faces challenges in developing durable TPS suitable for the vertical propulsive landing profile of the NGLV booster, building on prior reusable technology demonstrations. Current Indian materials for heat shields lag behind those and , where companies like have demonstrated boosters enduring dozens of flights through iterative advancements in ablative and metallic TPS. ISRO's efforts, constrained by budget limitations, prioritize cost-effective innovations but require further refinement to match the rapid turnaround and high-cycle reusability of international counterparts. Supply chain dependencies pose another significant obstacle, especially for and , which constitute about 10% of the vehicle's components despite 90% overall . ISRO relies on imported high-precision for guidance and control systems, increasing vulnerability to global disruptions and costs. Initiatives under aim to mitigate this by fostering domestic manufacturing, with ISRO Chairman V. Narayanan advocating for reduced imports through partnerships with Indian industry. Testing limitations further complicate NGLV development, as full-scale hot-fire facilities for semi-cryogenic engines and stages are maturing, with integrated stage tests expected to support the first flights around 2027-2028. Current infrastructure at the in Mahendragiri supports tests up to 2600 kN thrust via power head test articles, including recent successful hot tests of the semi-cryogenic power head in May 2025. Comprehensive stage-level evaluations rely on simulations and subscale models in the interim, introducing uncertainties in validating the LME1100 (~1100 kN) semi-cryogenic engine's performance for NGLV boosters. Integration challenges arise in human-rating the vehicle, which demands exceptionally high reliability standards to ensure crew safety during missions. For cryogenic stages, this requires rigorous qualification processes, as demonstrated by the successful human-rating of the engine through extensive endurance testing exceeding 6350 seconds of operation. Past anomalies in cryogenic upper stages, such as ignition failures, highlight the complexities of integrating these systems with abort mechanisms and escape systems, necessitating design modifications for fault-tolerant performance.

Strategic Importance

The Next Generation Launch Vehicle (NGLV) represents a pivotal advancement in India's space program, enabling the nation to achieve greater self-reliance in heavy-lift capabilities essential for strategic national objectives. With a payload capacity of up to 30 tonnes to (LEO)—three times that of the —it supports critical missions such as the Bharatiya Antariksh Station by 2035. As of November 2025, NGLV development continues alongside the Lunar Module Launch Vehicle (LMLV), an evolved heavier variant (up to 80 tonnes to LEO) targeted for an Indian crewed lunar landing by 2040, advancing and interplanetary exploration. This enhanced capacity addresses the evolving demands of satellite constellations, , and scientific missions, reducing dependence on foreign launch services and bolstering India's in space activities. Strategically, the NGLV's partially reusable design, featuring a recoverable first stage, is projected to lower costs per to by approximately half compared to current expendable vehicles, fostering a cost-efficient for both and commercial operations. This reusability not only democratizes access to but also stimulates through increased private sector involvement, job creation in high-technology , and integration with initiatives like Space Vision 2047. By enabling higher launch frequencies and supporting defense-oriented applications—such as secure communications and maritime surveillance—the vehicle strengthens in an increasingly contested domain. On the global stage, the NGLV positions as a competitive player in the international space economy, facilitating collaborations like the NASA-ISRO (NISAR) mission and potential partnerships for lunar sample returns. Its development underscores India's commitment to innovation, with the reusable technology marking a 1,000-fold increase in capability since the SLV-3 era, thereby enhancing geopolitical influence and technological leadership. Overall, the NGLV is integral to realizing ambitious goals like orbiter missions and Chandrayaan-4, ensuring sustainable progress in space exploration while aligning with broader .

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