Vertical takeoff vertical landing (VTVL) guidance and control
ISRO has demonstrated autonomous VTVL guidance and control for winged vehicles but is still developing retro-propulsive booster recovery capability.
| India's status | Demonstrated since 2026 |
|---|---|
| Criticality | high |
| Global makers | 3 United States · China · India |
| Type | software |
| Sector | Space Systems |
| Rests on | 8 capabilities |
| Deep-red gaps | 1 |
| Verification | Machine-checked |
| Revised | 2026-07-15 |
1The gap
Does India have vertical takeoff and vertical landing guidance for rockets?
Reusing a rocket stage instead of discarding it lowers launch cost by 5 to 20 times. The software that makes reuse possible — guiding a booster from hypersonic descent to a pinpoint upright touchdown — is held by only three nations: the United States, China and India.
The hard part is not the engine. It is the guidance. A returning stage must predict its own trajectory in real time, correct for wind and cross-range error, and command thrust and steering surfaces down to the last metre — all autonomously, with no human in the loop. Cold gas thrusters trim attitude, grid fins steer through the atmosphere, and a re-ignitable, throttleable engine arrests the fall. The onboard navigation, guidance and control system must fuse all of this fast enough to survive a descent from hypersonic speed.
India has demonstrated the guidance half of this problem on a winged vehicle. ISRO completed three consecutive autonomous landing experiments — RLV LEX-01 through LEX-03 — with the RLV-TD, beginning with the 2 April 2023 release from 4.5 km altitude. The final test, RLV LEX-03 on 23 June 2024 at the Aeronautical Test Range in Chitradurga, re-demonstrated autonomous landing under harder conditions: 500 metres of cross-range against 150 for LEX-02, and more severe winds. The integrated navigation, guidance and control system held.
What India has not yet demonstrated is retro-propulsive booster recovery — the vertical descent under engine thrust that SpaceX first achieved with a Falcon 9 in December 2015, and has since repeated across more than 500 booster recoveries at reuse rates above 90 percent. ISRO is developing this separately through ADMIRE, a test bed for vertical landing technology aimed at retro-propulsion capabilities comparable to the Falcon 9.
The gap persists because winged landing and retro-propulsive landing are different control problems. A gliding vehicle bleeds energy aerodynamically; a booster must balance on its own thrust, a fundamentally harder stabilisation task. The foundational pieces — inertial navigation, throttleable restartable engines, cold gas reaction control, deployable landing legs — are in production or demonstrated. What remains is integrating them into a single autonomous descent.
2Tech tree
read left to right · click any card for its record3The builders
Stage = IndiaBUILD assessment from evidence4What it would take
Closing the gap runs through the Next Generation Launch Vehicle, designed to replace the PSLV with a reusable first stage using vertical landing technology. Vikram Sarabhai Space Centre is developing the steerable grid fins, deployable legs and advanced avionics required. The longer aim is a fully reusable two-stage-to-orbit system — the point at which demonstrated guidance becomes routine, recoverable flight.
The diagnosis is free. The argument, the politics, and the case — in Swarajya.
- ISRO Completes RLV Technology Demonstrations RLV-LEX3(contested)
- ISRO Completes RLV Technology Demonstrations RLV-LEX3
- Parliament Question: Development of Reusable Launch Vehicle Technology
- Reusable Launch Vehicle (RLV) Technology
- Next Generation Launch Vehicle
- VTVL — Grokipedia(contested)
- VTVL — Grokipedia
- VTVL — Wikipedia(contested)
- Reusable Launch Vehicle Autonomous Landing Mission (RLV LEX)(contested)
- Reusable Launch Vehicle (RLV) Technology
- RLV Technology Demonstration Programme
- Reusable Launch Vehicle (RLV) Technology
- India's Reusable Space Plane: Progress and Potential
- India Type Certification Guidance for VTOL-Capable Aircraft