RLV-TD

Reusable Launch Vehicle - Technology Demonstrator (RLV-TD) is one of the most technologically
challenging endeavors of ISRO towards developing essential technologies for a fully reusable launch
vehicle to enable low cost access to space. The configuration of RLV-TD is similar to that of an
aircraft and combines the complexity of both launch vehicles and aircraft. The winged RLV-TD has
been configured to act as a flying test bed to evaluate various technologies, namely, hypersonic
flight, autonomous landing and powered cruise flight. In future, this vehicle will be scaled up to
become the first stage of India's reusable two stage orbital launch vehicle.
RLV-TD consists of a fuselage (body), a nose cap, double delta wings and twin vertical tails. It also features symmetrically placed active control surfaces called Elevons and Rudder. This technology demonstrator was boosted to Mach no: 5 by a conventional solid booster (HS9) designed for low burn rate. The selection of materials like special alloys, composites and insulation materials for developing an RLV-TD and the crafting of its parts is very complex and demands highly skilled manpower. Many high technology machinery and test equipment were utilised for building this vehicle.
RLV-TD consists of a fuselage (body), a nose cap, double delta wings and twin vertical tails. It also features symmetrically placed active control surfaces called Elevons and Rudder. This technology demonstrator was boosted to Mach no: 5 by a conventional solid booster (HS9) designed for low burn rate. The selection of materials like special alloys, composites and insulation materials for developing an RLV-TD and the crafting of its parts is very complex and demands highly skilled manpower. Many high technology machinery and test equipment were utilised for building this vehicle.
RLV-TD Specifications
Feature | Specification/Description |
---|---|
Vehicle Type | Reusable Spaceplane |
Launch Agency | ISRO |
Objectives |
|
Propulsion System | Scramjet propulsion (possible) |
Wings | Winged body design for controlled descent |
Launch Status | Technology Demonstrator (Experimental) |
Current Status | Ongoing development/testing (as of 2022) |
Notable Achievements | (List any notable achievements or tests) |
Mission Profile


Data Communication

