


India has been steadily advancing its space capabilities over the past several decades, with ambitious goals of developing reusable launch vehicles to reduce the costs of accessing space. At the forefront of these efforts is the Reusable Launch Vehicle – Technology Demonstrator (RLV-TD) program, which has been making significant strides in recent years. This article examines the development, current status, and future prospects of India’s reusable space plane technology.
Background and Motivation
The Need for Reusable Launch Vehicles
Space launches have traditionally relied on expendable rockets that are discarded after a single use. This approach results in high costs, as entirely new vehicles must be manufactured for each mission. Reusable launch vehicles offer the potential to dramatically reduce these costs by allowing key components to be recovered and reused multiple times.
ISRO’s Vision
The Indian Space Research Organisation (ISRO) recognized the importance of developing reusable technology to maintain India’s competitiveness in the global space industry. In the early 2000s, ISRO began conceptual work on a reusable launch vehicle, with the goal of eventually creating a fully reusable two-stage-to-orbit (TSTO) system.
The RLV-TD Program

Program Overview
The Reusable Launch Vehicle – Technology Demonstrator (RLV-TD) program was officially initiated by ISRO in 2012. Its purpose is to develop and demonstrate the technologies required for a reusable space transportation system. The RLV-TD itself is a scaled-down prototype, about 6.5 meters long, used to test various aspects of reusable vehicle design and operation.
Key Technologies
The RLV-TD program focuses on several critical technologies:
- Hypersonic flight
- Autonomous landing
- Powered cruise flight
- Hypersonic flight with air-breathing propulsion
Phased Approach
ISRO adopted a phased approach for the RLV-TD program, with multiple planned missions to incrementally test different aspects of reusable vehicle technology:
- Hypersonic Flight Experiment (HEX)
- Landing Experiment (LEX)
- Return Flight Experiment (REX)
- Scramjet Propulsion Experiment (SPEX)
Major Milestones and Achievements
HEX Mission (2016)

The first major test of the RLV-TD program was the Hypersonic Flight Experiment (HEX), conducted on May 23, 2016. In this mission, the RLV-TD was launched atop a HS9 solid rocket booster to an altitude of about 65 km. The vehicle then performed a controlled descent, reaching hypersonic speeds (Mach 5+) before splashing down in the Bay of Bengal.
Key accomplishments of the HEX mission included:
- Successful separation of the RLV-TD from the booster
- Demonstration of aerodynamic stability at hypersonic speeds
- Validation of thermal protection systems
- Collection of data on hypersonic flight characteristics
LEX Missions (2023-2024)
The Landing Experiment (LEX) phase of the program focused on demonstrating autonomous landing capabilities. Unlike the HEX mission, these tests did not involve rocket launches. Instead, the RLV-TD prototype (nicknamed “Pushpak”) was carried to altitude by helicopter and released to perform autonomous approach and landing maneuvers.
LEX-01 (April 2023)
The first LEX mission took place on April 2, 2023. Key details include:
- Release altitude: 4.5 km
- Landing site: Aeronautical Test Range, Chitradurga, Karnataka
- Successful demonstration of autonomous navigation, approach, and landing
LEX-02 (March 2024)
The second LEX mission, conducted on March 22, 2024, built upon the success of the first:
- More challenging release conditions
- Demonstration of cross-range and downrange corrections
- Reuse of the same vehicle from LEX-01, showcasing reusability
LEX-03 (June 2024)
The third and final LEX mission occurred on June 23, 2024:
- Further increased difficulty in release conditions and wind
- Larger cross-range error to correct (500 m vs 150 m in LEX-02)
- Successful completion of the LEX phase of the program
Current Status of the RLV-TD Program
Technology Readiness
With the completion of the LEX phase, ISRO has demonstrated several key technologies required for a reusable launch vehicle:
- Hypersonic flight control
- Thermal protection systems
- Autonomous navigation and landing
- Reusability of vehicle components
Remaining Challenges
While significant progress has been made, several challenges remain before a fully operational reusable launch vehicle can be realized:
- Powered flight and propulsion systems for ascent
- Air-breathing propulsion for atmospheric flight
- Full-scale vehicle design and integration
- Rapid turnaround and refurbishment procedures
Next Steps: The Orbital Re-entry Vehicle
ORV Overview
With the success of the RLV-TD experiments, ISRO is now preparing for the next phase of development: the Orbital Re-entry Vehicle (ORV). This will be a larger, more capable vehicle designed to reach orbit and return safely to Earth.
Key Features
The planned ORV will have several advancements over the RLV-TD:
- Approximately 1.6 times larger than the RLV-TD
- Capable of reaching a 400 km orbit
- Equipped with a heat shield for atmospheric re-entry
- Featuring a foldable landing gear system
Launch Plans
ISRO intends to launch the ORV within the next two years, using a modified Geosynchronous Satellite Launch Vehicle (GSLV). This mission will serve as a critical test of technologies required for a fully operational reusable launch system.
Potential Applications and Benefits
Cost Reduction
The primary motivation for developing reusable launch vehicles is to reduce the cost of access to space. By reusing major components, particularly the first stage of a launch vehicle, costs could potentially be reduced by 30-40%.
Increased Launch Frequency
Reusable vehicles could enable a higher frequency of launches, as the time and resources required to prepare for each mission would be significantly reduced.
Flexibility and Responsiveness
A reusable system could offer greater flexibility in mission planning and execution, allowing for more responsive space access to meet evolving needs.
Technology Spin-offs
The development of reusable space vehicles drives advancements in materials science, propulsion, avionics, and other fields, with potential applications beyond the space sector.
Comparison to International Efforts
United States
- NASA’s Space Shuttle (retired): The most famous reusable spacecraft program, operating from 1981 to 2011.
- X-37B: An uncrewed, reusable space plane operated by the U.S. Air Force.
- Dream Chaser: An uncrewed, reusable space plane operated by Sierra Space.
Russia
- Energia-Buran: A Space Shuttle-like system that flew only once in 1988.
Europe
- Space Rider: A reusable spaceplane being developed by the European Space Agency.
China
- CSSHQ: An uncrewed, reusable space plane similar to the X-37.
Challenges and Considerations
Technical Complexities
Developing a fully reusable launch system presents numerous technical challenges, including:
- Managing the extreme temperatures and stresses of atmospheric re-entry
- Achieving the necessary precision for vertical landings or runway touchdowns
- Designing robust, reusable engines capable of multiple firings
Economic Viability
While reusability promises cost savings, the economics are complex:
- High upfront development costs
- Need for a sufficient launch cadence to justify reusability investments
- Balancing payload capacity with the mass penalties of reusable systems
Operational Considerations
Reusable systems introduce new operational challenges:
- Rapid inspection and refurbishment between flights
- Managing a fleet of reusable vehicles
- Adapting launch infrastructure and procedures
Policy and Regulatory Issues
The introduction of reusable launch vehicles may require updates to existing space policies and regulations, both domestically and internationally.
Future Outlook
Short-term Goals
In the near future, ISRO will focus on:
- Conducting the Orbital Re-entry Vehicle (ORV) mission
- Further refining autonomous landing capabilities
- Developing and testing air-breathing propulsion systems
Medium-term Objectives
Looking ahead 5-10 years, potential objectives include:
- Demonstrating end-to-end reusability (launch to landing)
- Scaling up to a full-size reusable first stage
- Exploring potential commercial applications of the technology
Long-term Vision
ISRO’s ultimate goal is to develop a fully reusable two-stage-to-orbit (TSTO) launch system. This would represent a major leap in space access capabilities, potentially revolutionizing India’s space program and its role in the global space industry.
Summary
India’s pursuit of reusable space plane technology through the RLV-TD program represents a significant commitment to advancing its space capabilities. The successful completion of the Landing Experiment (LEX) phase marks an important milestone, demonstrating key technologies required for autonomous, reusable space vehicles.
As ISRO moves forward with plans for an Orbital Re-entry Vehicle and continues to refine its designs, India is positioning itself as a serious contender in the development of next-generation space transportation systems. While challenges remain, the progress made thus far is impressive and holds promise for the future of India’s space program.
The development of reusable launch vehicles has the potential to dramatically reduce the costs of accessing space, opening up new possibilities for scientific research, commercial applications, and space exploration. As India continues to advance this technology, it may play an increasingly important role in shaping the future of global space activities.

