ISRO successfully launches ‘Reusable Launch Vehicle Autonomous Landing Mission’ | DETAILS

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ISRO successfully launches ‘Reusable Launch Vehicle Autonomous Landing Mission’ | DETAILS


Image Source : TWITTER ISRO successfully launches ‘Reusable Launch Vehicle Autonomous Landing Mission’

The Indian Space Research Organisation (ISRO) successfully performed the ‘Reusable Launch Vehicle Autonomous Landing Mission’ (RLV LEX) on Sunday morning. The check was performed on the Aeronautical Test Range (ATR) at Chitradurga, Karnataka within the early hours of April 2. 

The RLV took off at 7:10 am IST by a Chinook Helicopter of the Indian Air Force as an underslung load and flew to a top of 4.5 km. Once the predetermined pillbox parameters have been attained, primarily based on the RV’s Mission Management Computer command, the RV was launched in mid-air, at a down vary of 4.6 km.

Release circumstances included 10 parameters protecting place, velocity, altitude and physique charges, and many others. The launch of RLY was autonomous. RLY then carried out method and touchdown manoeuvres utilizing the Integrated Navigation, Guidance & management system and accomplished an autonomous touchdown on the AlK on the strip at 7:40 AM IST. With that, ISRO successfully achieved the autonomous touchdown of an area automobile.

How touchdown was carried out? 

The autonomous touchdown was carried out beneath the precise circumstances of a Space re-entry automobile’s touchdown high-speed, unmanned, exact touchdown from the identical


return path because it the automobile arrives from area.

Landing parameters reminiscent of Ground relative velocity, the sink price of Landing Gears, and exact physique charges, as is perhaps skilled by an orbital re-entry area automobile in its return path, have been achieved.

The RL LEX demanded a number of state-of-the-art applied sciences together with correct Navigation {hardware} and software program, Pseudolite system, Ka-band Rada:

Altimeter, NavIC receiver, indigenous Landing Gear, Aerofoil honey-comb fins and brake parachute system. 

Winged physique carried by helicopter

In a primary on the earth, a winged physique has been carried to an altitude of 4.5 km by helicopter and launched for finishing up an autonomous touchdown on a runway. RLV is actually an area aircraft with a low lift-to-drag ratio requiring an method at excessive glide angles that necessitated a touchdown at excessive velocities of 350 kmph.

LEX make the most of a number of indigenous programs. Localized Navigation programs primarily based on pseudolite programs, instrumentation, and sensor programs, and many others. have been developed by ISRO. 

Digital Elevation Model (DEM) of the touchdown website with a Ka-band Radar Altimeter offered correct altitude info. Extensive wind tunnel assessments and CFD

simulations enabled aerodynamic characterization of RL previous to the flight Adaptation of up to date applied sciences developed for RV LEX turns different operational launch automobiles ofISRO cheaper.

ISRO had demonstrated the re-entry of its winged automobile RLV-TD within the HEX mission in May 2016. The re-entry of a hypersonic sub-orbital automobile marked : main accomplishment in creating Reusable Launch Vehicles.

ALSO READ: Indian Space Research Organisation launches India’s largest LVM3 rocket carrying 36 satellites

LEX mission achieves closing method section

In HEX, the automobile landed on a hypothetical runway over the Bay of Bengal. Precise touchdown or a runway was a side not included within the HEX mission. The LEX mission achieved the ultimate method section that coincided with the re-entry return flight path exhibiting an autonomous, high-speed (350 kmph) touchdown.

The LEX started with an Integrated Navigation check in 2019 and adopted a number of Engineering Model Trials and Captive Phase assessments in subsequent years.

Along with ISRO, IAF, CEMILAC, ADE, and ADRDE contributed to this check. The IAF staff hand in hand with the Project staff and a number of sorties have been performed te good the achievement of launch circumstances. Dr. S Unnikrishnan Nair, Director, VSSC, and Shri Shyam Mohan N, Programme Director, A TSP guided the groups. 

Dr. Jayakumar M, Project Director, RV was the Mission Director, and Shri Muthupandian J, Associate Project Director, RL was the Vehicle Director for the mission. Meanwhile, Ramakrishna, Director, ISTRAC was additionally current on the event.

Chairman, ISRO/Secretary, DOS Shri S Somanath witnessed the check and congratulated the staff. With LEX, the dream of an Indian Reusable Launch Vehicle comes one step nearer. 

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