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First pic of RLV-TD : Reusable Launch Vehicle to take off next week

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ISRO_2856109f.jpg



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The technology demonstrator will take place from Satish Dhawan Space Centre in Sriharikota.
The first technology demonstrator (TD) launch of the Indian Space Research Organisation’s Reusable Launch Vehicle (RLV), or the spaceplane in popular parlance, will take place on May 23 at 9.30 a.m. from the Satish Dhawan Space Centre (SDSC), Sriharikota, according to ISRO officials.

Visually, the RLV-TD is a rocket-aircraft combination measuring about 17 m, whose first stage is a solid propellant booster rocket and the second stage is a 6.5 m long aircraft-like winged structure sitting atop the rocket.

A misnomer

However, the popular perception of the technology as a marriage between rocket and aircraft is a misnomer.

In RLV-TD that is awaiting launch at SHAR, the first stage, weighing about 9 tonnes, is merely the Satellite Launch Vehicle (SLV-3) flown in the 1980s.

The vehicle will take off like a rocket and the RLV will be taken to a height of 70 km and where the booster will release the vehicle to carry out its manoeuvres.

Hypersonic Experiment 1

According to Dr. K. Sivan, director of the Vikram Sarabhai Space Centre (VSSC), Thiruvanathapuram, where the RLV was designed, assembled and where it underwent basic electrical, hydraulic and “sign check” tests, the objective is to achieve hypersonic speeds to basically test the hypersonic aero-thermodynamic characterisation of the winged body’s re-entry, its control and guidance systems, autonomous mission management to land at a specific location at sea and testing of “hot structures” that make up the structure of the RLV.

The test is, therefore, termed as Hypersonic Experiment 1 (HEX-1).

Complex technology

A conventional launch vehicle (LV), says Dr. Sivan, spends the lowest time of its flight in the atmosphere, whereas the RLV system spends all the time in the atmosphere. Also, while an aircraft experiences limited flight regime of say Mach 0 to Mach 2 or so, the RLV experiences a much wider range of flight regimes.

Hence the technology of an RLV is much more complex basically arising from the design of the control and guidance systems, he pointed out.

In HEX1, the winged RLV is otherwise a dummy with no powered flight of its own. In this test, the RLV will attain a flight regime of Mach 5 with the help of the booster alone, Dr. Sivan said. At the end of the HEX1 mission, the aircraft will land in sea. The total flight duration of the RLV-TD from launch till splash down will be about 10 mins.

However, the ultimate objective of the RLV programme of ISRO is to enable the vehicle traverse a very wide range of flight regimes from Mach 0 to Mach 25 based on air-breathing propulsion for achieving two-stage-to-orbit (TSTO) launch capability.

The integrated test system (booster plus the RLV-TD) is already at the SDSC (SDSC), Sriharikota. Prior to being moved to Sriharikota, the RLV subsystem underwent acoustic tests at the National Aerospace Laboratories of the CSIR (CSIR-NAL) and the booster went as a separate subsystem directly from VSSC. At SDSC the two were mated together.

Dr. A.S. Kiran Kumar, ISRO Chairman, called the first test launch HEX1 “a very preliminary step” and stressed that “we have to go a long way” before it could be called a re-usable launch system. “But these are very essential steps we have to take,” he said.

Lower cost

Asked whether the Indian reusable launch system was aimed at bringing down the launch cost, the ISRO Chairman said, “It will bring down the cost. Towards that, we will have to work and go through these initial steps,” the Chairman said.

Flying test bed

The present design is basically “a flying test bed to evaluate various technologies, namely hypersonic flight, autonomous landing, powered cruise flight and hypersonic flight using air-breathing propulsion using a scramjet engine”, according to ISRO website.

The HEX series of experiments will be followed by the landing experiment (LEX), return flight experiment and scramjet propulsion experiment (SPEX).

The basic design of a scramjet has already been evolved.

A test launch of the engine aboard a sounding rocket, which will achieve a flight regime of up to Mach 8, will take place some place in June at SHAR, Dr. Sivan said.
://www.thehindu.com/multimedia/dynamic/02856/ISRO_2856109f.jpg
 
WOHOOOOO!! ISROOOOO ISROOO!! ISSRRROOOOOO !! ISSSROOOOOOO!!!
 
There she lies waiting for her maiden experimental flight :woot:
 
Great news.... I want to know while it's return are they going to land it on a run way or dump it on the ocean
 
Great news.... I want to know while it's return are they going to land it on a run way or dump it on the ocean
They'll have to crash it in sea as it would need a 4-5 km long runway to land which they lack near testing site.....ISRO is planning to build a 4-5 km long runway near sri harikota though...(only in future)
 
Very impressive. ISRO and India's space program has come a long way since its humble beginnings. The RLV-TD will make India the fourth nation to test such a concept.

Will the vehicle have its own power for its ascent, or is it provided by the booster?
 
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Very impressive. ISRO and India's space program has come a long way since its humble beginnings. I believe the RLV-TD will make India the third nation in the world to test such a concept.

Will the vehicle have its own power for its ascent, or is it provided by the booster?

A booster will be there which will be separated later

RLV-TDV.jpg
 
Thank you.

I suspect later variants will include their own propulsion as well as a possible two-man crew configuration, which would still within the payload range of the GSLV Mk.III launch vehicle.

you are absolutely right, later variants will have their own propulsion system.

it's a phased development

Phased Development
Reusable Launch Vehicle technology will be developed in phases through a series of trial flights.

The first in the series of trials is the hypersonic flight experiment (HEX) followed by the landing experiment (LEX), return flight experiment (REX) and scramjet propulsion experiment (SPEX).

Hypersonic Flight Experiment (HEX)
Flight testing will start with RLV-TD (HEX). During the mission, a booster rocket (Single strap-on solid booster of the Polar Satellite Launch Vehicle (PSLV) with 9 tonne fuel.) will take the 1.5 tonne RLV 1/6 scale model to 70-km altitude and release it. The booster rocket will fall back into the sea. [via TNIE]

The lofted RLV will re-enter the atmosphere independently travelling at around 2-km / sec. The descent speed would be controlled using the fins. The RLV has protective tiles to dissipate frictional heat during re-entry.

In the first trial-flight, the RLV will not be recovered from sea because it will not be cost-effective to do so. ISRO will instead use telemetry data data on the re-entry, deceleration and return.


Landing Experiment (LEX)
In the second phase RLV will be tested without its scramjet engine. After burnout, the booster will separate and fall away, and the RLV-TD will go on to make an unpowered ascent.

The RLV-TD will then re-enter the atmosphere at hypersonic speed and use aerodynamic breaking to decelerate. It will perform a range maneuver at 15-km, a 2g turn towards its launch site. Once the TD reaches 0.8 M, it will light up a turbofan engine to cruise back to its launch site at 0.6M and make a horizontal landing on a runway.

Return Flight Experiment (REX)
In this phase, the RLV-TD will be launched to orbit and then de-orbited for a landing on a runway.

Scramjet Propulsion Experiment (SPEX)
Eventually, the RLV will be powered by an air breathing scram jet which is being developed under a separate project called
Air Breathing Propulsion Project (ABPP).
 

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