ISRO
India plays leading roll in space research now the next mission in launching vehicle is taken by ISRO which RLV. THhe world knows, ISRO make a heavy mission possible with low cost and less period of time. Now, the technological view of our scientist, improving the level of launching vehicle to make it reusable one.
This mission is like to maken a prototype launch on april 16 but which is postborne to coming year 2016.
RLV-TD
India plays leading roll in space research now the next mission in launching vehicle is taken by ISRO which RLV. THhe world knows, ISRO make a heavy mission possible with low cost and less period of time. Now, the technological view of our scientist, improving the level of launching vehicle to make it reusable one.
This mission is like to maken a prototype launch on april 16 but which is postborne to coming year 2016.
RLV-TD
The cost of access to space is the major deterrent
in space exploration and space utilization. A reusable launch vehicle
is the unanimous solution to achieve low cost, reliable and on-demand
space access.
Reusable Launch Vehicle-Technology Demonstration
Program or RLV-TD is a series of technology demonstration missions that
have been considered as a first step towards realizing a Two Stage To
Orbit (TSTO) fully re-usable vehicle. A Winged Reusable Launch Vehicle
technology Demonstrator (RLV-TD) has been configured to act as a flying
test bed to evaluate various technologies, namely, hypersonic flight,
autonomous landing, powered cruise flight and hypersonic flight using
air-breathing propulsion.
These technologies will be developed in phases
through a series of experimental flights. The first in the series of
experimental flights is the hypersonic flight experiment (HEX) followed
by the landing experiment (LEX), return flight experiment (REX) and
scramjet propulsion experiment (SPEX). Reusable Launch Vehicle
Technology Demonstrator Hypersonic Experiment (RLV-TD HEX1) wherein the
hypersonic aero-thermo dynamic characterization of winged re-entry body
along with autonomous mission management to land at a specified location
and characterization of hot structures are planned to be demonstrated.
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