GS Paper: GS3-17.Awareness in the fields of IT, Space, Computers, Robotics, Nano-technology, Bio-technology and issues relating to Intellectual Property Rights.

Why in the News:

Skyroot Aerospace’s Vikram-1 successfully reached orbit, becoming the first India based private company to independently develop and launch an orbital rocket. With this achievement, India joins the United States and China as the only countries where a private company has achieved an orbital launch, six years after opening the space sector to private participation.

What does the Vikram-1 launch signify about India’s position in the global private space sector?

1. Exclusive club: India becomes only the third country after the United States and China where a private company has independently developed and launched an orbital rocket.
2. Policy milestone: The achievement follows the 2020 space sector reforms, later institutionalised through the Indian Space Policy, 2023, which enabled greater participation by private players.
3. Expanding ecosystem: India now has around 400 space start ups working across the space value chain, including launch vehicles, satellites, space electronics, and downstream applications.
4. Growth potential: India’s space sector is valued at around Rs 70,000 crore, with the government projecting four to five times growth over the next decade.

Why does the launch matter specifically for Low Earth Orbit (LEO), and what does that free ISRO to do?

1. Emerging commercial market: The rapid increase in small satellites weighing from a few kilograms to a few hundred kilograms has created a fast growing commercial launch market, beyond the capacity of any single national space agency.
   • Term: Low Earth Orbit (LEO): The region of space located approximately 160 km to 2,000 km above Earth’s surface, where most modern communication, Earth observation, and small satellite missions operate.
2. Division of responsibilities: As private companies undertake commercial satellite launches, ISRO can increasingly focus on high value scientific and strategic missions such as Chandrayaan, Gaganyaan, and future deep space exploration programmes.

Does private launch capability mean independence from ISRO, or a different kind of dependency?

1. Continued role of ISRO: The development of Vikram-1 relied significantly on ISRO’s infrastructure, testing facilities, and ecosystem, demonstrating a public private partnership model rather than complete private independence.
2. India’s distinct model: Unlike the United States, where companies such as SpaceX independently develop technologies before partnering with NASA, India’s private space sector is expected to remain closely linked with ISRO for the foreseeable future.
3. Competitive advantage: Indian companies like Skyroot Aerospace are expected to compete globally by leveraging India’s strengths in cost effective engineering, frugal innovation, and efficient manufacturing.
4. Commercial challenges: The failures of companies such as Vector Launch and Virgin Orbit highlight the high financial risks and competitive nature of the commercial launch industry.

Conclusion:

The successful launch of Vikram-1 marks a major milestone in India’s transition towards a vibrant private space ecosystem, demonstrating the impact of the 2020 space reforms and the Indian Space Policy, 2023. While the achievement reflects the growing capability of Indian private industry, it also underscores the continuing importance of ISRO’s institutional support. Going forward, the long term success of India’s private space sector will depend on its ability to build commercially sustainable business models, expand global launch services, and strengthen public private collaboration in an increasingly competitive global space economy.

Why in the News?

India’s Human-rated Launch Vehicle Mark-3 (HLVM3) will place the Gaganyaan Orbital Module, carrying Indian astronauts, into orbit for the country’s maiden crewed space mission. The astronauts’ survival on return depends on the crew module’s re-entry design, which must balance competing engineering demands that no single shape can satisfy at once.

How is the Gaganyaan Orbital Module structured for the crew’s return journey?

1. Two-module design: The Orbital Module (OM) has two sections, the crew module and the service module, connected by a joint.
2. Division of function: The crew module serves as the crew habitat. The service module provides on-orbit support to the OM.
3. De-orbit sequence: The service module’s propulsion system fires thrusters to de-orbit the OM. The service module then separates from the crew module through a redundant severing mechanism.
4. Differential survival: The crew module is built to survive re-entry heat loads. It decelerates through aero-braking (Aero-braking: use of atmospheric drag to slow a spacecraft during descent) and splashes down in the sea. The service module burns up during descent.

Why is there no single “ideal” shape for a re-entry crew module?

1. Competing design objectives: A crew module must simultaneously maximise internal volume, manage aerodynamic lift and drag, stay easy to fabricate, maintain aerodynamic and hydrodynamic stability, and stabilise dynamically at low speeds.
2. No configuration satisfies all objectives: No single shape meets every requirement at once. The final shape depends on which objectives are prioritised.
3. Mass-minimisation strategy: Engineers strip the module to essential landing systems to minimise launch and re-entry mass. This directly reduces the size and mass of the heatshield and parachutes.
4. The sphere’s trade-off: A sphere offers the maximum internal volume for the minimum structural mass, since a sphere has the smallest surface area for a given volume. A sphere also generates no aerodynamic lift, so it falls straight down and subjects the crew to high g-forces.
5. The sphere-cone compromise: A sphere-cone configuration is preferred for re-entry. Its blunt base creates a detached shockwave that pushes frictional heat away from the spacecraft. Its conical body provides the lift and aerodynamic stability needed for a controlled descent. The Gaganyaan crew module uses this sphere-cone configuration.

What do other crewed spacecraft designs show about configuration choices?

1. Russia’s Soyuz and China’s Shenzhou: Both use a three-module configuration. This adds a dedicated third module for extra living and working space, unlike Gaganyaan’s two-module OM.
2. Function of the third module: This module houses the docking mechanism, cargo, and basic life-support facilities, including the toilet. It separates and is destroyed during re-entry, like the service module.
3. Soviet Union’s Vostok: The Vostok capsule, in which Yuri Gagarin made the first human spaceflight, used the design closest to a perfect sphere among crewed capsules.
4. Design lesson: Vostok’s near-spherical shape shows the volume-versus-lift trade-off directly. It maximised internal volume but sacrificed aerodynamic lift, the same trade-off Gaganyaan’s engineers manage through the sphere-cone choice.

Why does even an optimised sphere-cone shape fail to guarantee stability?

1. Mono-stability defined: A module is aerodynamically mono-stable if it holds only one stable attitude while flying through the atmosphere, similar to a shuttlecock. Hydrodynamic mono-stability means the module self-rights into a single stable orientation after splashdown.
2. What controls mono-stability: Mono-stability depends on the module’s aerodynamic shape and the location of its centre of gravity.
3. The packaging constraint: The centre of gravity is fixed by how internal subsystems are packed. System engineers often cannot freely relocate it to the position mono-stability requires.
4. Result-multiple stable orientations: Most modules end up with more than one stable orientation. The Gaganyaan crew module has two stable aerodynamic positions and two stable hydrodynamic positions.
5. Active correction, not passive design: The undesired attitude is corrected using control thrusters during atmospheric flight and a gas-based up-righting system after splashdown, not through shape alone.

What makes dynamic instability the most dangerous phase of re-entry?

1. Dynamic instability defined: Dynamic instability is a condition in which a re-entry module develops rapidly growing, uncontrolled oscillations as it decelerates through the atmosphere.
2. The kite analogy: A kite without a tail wobbles and spins out of control because it lacks stability. A crew module without correction can develop similar self-growing, tumbling swings.
3. Peak danger zone: The module shakes and wobbles most as it approaches the speed of sound, where bouncing shockwaves and swirling air violently disturb it.
4. Mitigation tools: Small control thrusters steady the module, or parachutes deploy, before the instability grows too large.

Conclusion

No re-entry module design can be geometrically stable and volume-efficient at once. Every shape choice trades one property for another. Gaganyaan’s sphere-cone crew module manages this trade-off rather than eliminating it, relying on control thrusters, a gas-based up-righting system, and parachutes to correct the multiple stable orientations and dynamic oscillations that the shape alone cannot resolve. Passive aerodynamic design sets the outer limits of what is survivable; active control systems close the remaining gap to a safe splashdown.

PYQ Relevance

[UPSC 2017] India has achieved remarkable successes in unmanned space missions including the Chandrayaan and Mars Orbiter Mission, but has not ventured into manned space mission. What are the main obstacles to launching a manned space mission, both in terms of technology and logistics? Examine critically.

Linkage: The PYQ examines the technological and logistical challenges of India’s human spaceflight programme. The article explains how Gaganyaan’s crew module addresses key re-entry, safety, and recovery challenges, showcasing India’s progress towards successful human spaceflight.