Hypersonic Flight Experiment

Hypersonic Flight Experiment
Mission type Test flight
Operator ISRO
Mission duration 2 minutes
Start of mission
Launch date May 2016 (planned)[1]
Launch site Satish Dhawan FLP
End of mission
Landing site Bay of Bengal

Hypersonic Flight Experiment or HEX is planned to be the first test flight in the RLV-TD development program. The demonstration trials will pave the way for a Two-Stage-To-Orbit (TSTO) fully re-usable launch vehicle. HEX is scheduled for May 2016.[1]

Configuration

Model of RLV-TD launch arrangement

Objectives

HEX will be the first test flight of a reusable launch vehicle. The test flight objectives include:[2]

Flight

The HEX sits atop a 9 ton solid booster(S-9) which will propel the vehicle to a predetermined altitude. The first stage is then jettisoned and the vehicle re-enters the atmosphere at hypersonic speed. The vehicle gradually glides through the atmosphere and a parachute is deployed. The vehicle is then recovered from the sea.[2]

Current status

As of 2009, Airframe Engineering model, axisymmetric proto nose cap after graphitisation (C-C) and slow burn rate propellant were realized. Aerodynamic characterization of technology demonstration vehicle was completed at NAL, VSSC and IIST.

Computational flow simulation and supersonic combustion in ground testing have been successfully achieved. Scramjet engine modules (passive) for the DMRJ flight demonstration were realised and alignment / integration with the test vehicle is progressing. Real time decision based ignition of second stage, a first of its kind is ready for implementation in the test flight.[3]

ISRO has tentatively slated the HEX from the first launchpad of Satish Dhawan Space Centre for May 2016.[1]

See also

References

External links

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