Bengaluru (PTI): The Indian Space Research Organisation on Sunday successfully conducted the Reusable Launch Vehicle Autonomous Landing Mission (RLV LEX).

The test was conducted at the Aeronautical Test Range (ATR), Chitradurga, Karnataka, the national agency headquartered here said.

"With that, ISRO successfully achieved the autonomous landing of a space vehicle", it said in a statement.

"With LEX, the dream of an Indian Reusable Launch Vehicle arrives one step closer to reality", ISRO said.

In a first in the world, a winged body has been carried to an altitude of 4.5 km by a helicopter and released for carrying out an autonomous landing on a runway.

RLV is essentially a space plane with a low lift to drag ratio requiring an approach at high glide angles that necessitated a landing at high velocities of 350 kmph.

The RLV took off at 7:10 am IST by a Chinook Helicopter of the Indian Air Force (IAF) as an underslung load and flew to a height of 4.5 km (above Mean Sea Level).

Once the predetermined pillbox parameters were attained, based on the RLV's Mission Management Computer command, the RLV was released in mid-air, at a down range of 4.6 km.

Release conditions included 10 parameters covering position, velocity, altitude and body rates, etc. The release of RLV was autonomous. RLV then performed approach and landing maneuvers using the Integrated Navigation, Guidance & control system and completed an autonomous landing on the ATR air strip at 7:40 AM IST.

The autonomous landing was carried out under the exact conditions of a Space Re-entry vehicle's landing high speed, unmanned, precise landing from the same return path as if the vehicle arrives from space.

Landing parameters such as Ground relative velocity, the sink rate of Landing Gears, and precise body rates, as might be experienced by an orbital re-entry space vehicle in its return path, were achieved.

The RLV LEX demanded several state-of-the-art technologies including accurate Navigation hardware and software, Pseudolite system, Ka-band Radar Altimeter, NavIC receiver, indigenous Landing Gear, Aerofoil honey-comb fins and brake parachute system.

LEX utilised several indigenous systems. Localized Navigation systems based on pseudolite systems, instrumentation, and sensor systems, etc. were developed by ISRO.

Digital Elevation Model (DEM) of the landing site with a Ka-band Radar Altimeter provided accurate altitude information.

Extensive wind tunnel tests and CFD simulations enabled aerodynamic characterisation of RLV prior to the flight.

"Adaptation of contemporary technologies developed for RLV LEX turns other operational launch vehicles of ISRO more cost-effective", the statement said.

ISRO had demonstrated the re-entry of its winged vehicle RLV-TD in the HEX mission in May 2016. The re-entry of a hypersonic sub-orbital vehicle marked a major accomplishment in developing Reusable Launch Vehicles.

In HEX, the vehicle landed on a hypothetical runway over the Bay of Bengal. Precise landing on a runway was an aspect not included in the HEX mission.

The LEX mission achieved the final approach phase that coincided with the re-entry return flight path exhibiting an autonomous, high speed (350 kmph) landing.

The LEX began with an Integrated Navigation test in 2019 and followed multiple Engineering Model Trials and Captive Phase tests in subsequent years.

Along with ISRO, IAF, Centre for Military Airworthiness and Certification (CEMILAC), Aeronautical Development Establishment (ADE), and Aerial Delivery Research and Development Establishment (ADRDE) contributed to this test.

The IAF team hand in hand with the Project team and multiple sorties were conducted to perfect the achievement of release conditions.

Secretary in the Department of Space and ISRO Chairman S Somanath was among who witnessed the test.

 

Let the Truth be known. If you read VB and like VB, please be a VB Supporter and Help us deliver the Truth to one and all.



Hassan (Karnataka) (PTI): Karnataka Chief Minister Siddaramaiah on Saturday said that the Congress government led by him was ready to face the no-confidence motion if moved by the opposition during the legislature session from December 8.

With Deputy CM D K Shivakumar by his side, he reiterated that they would both abide by the high command's decision on the leadership issue.

"Let them (opposition) bring in a no-confidence motion or adjournment motion or any other motion. We are ready to face it. Ours is an open book, transparent government. We are ready to face anything," Siddaramaiah said in response to a question.

However, BJP state President B Y Vijayendra and Leader of Opposition in the Legislative Assembly R Ashoka, clarified that the party, along with the JD(S) has not discussed or decided anything so far regarding moving a no-confidence motion against the government.

ALSO READ: CM Siddaramaiah labels Kumaraswamy 'Manuvadi' over Bhagavad Gita curriculum push

The winter session of the Karnataka legislature will begin in Belagavi, bordering Maharashtra, on December 8 and will go on till 19th of this month.

Not wanting to react to a question on the leadership issue, the CM said the Congress high command is very strong.

"D K Shivakumar and I will be committed to whatever the high command decides," he said.

Earlier in the day in Bengaluru, Shivakumar accompanied AICC Mallikarjun Kharge till airport from Vidhana Soudha, after paying tributes to B R Ambedkar on his 69th death anniversary, which had led to some speculation about possible discussion between the two on the leadership issue.

The power tussle within the ruling party had intensified amid speculation about a change in chief minister in the state, after the Congress government reached the halfway mark of its five-year term on November 20.

However, both the CM and Deputy CM had recently held breakfast meetings at each others residences, on the instructions of the high command, which is seen as a move to pause the leadership tussle between the two and to signal Siddaramaiah's continuation as the CM for the time being, especially ahead of the Belagavi legislature session.