Author Topic: RLV-TD LEX-01, -02 and -03 (Landing Experiments)  (Read 52588 times)

Offline sanman

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RLV-TD LEX-01, -02 and -03 (Landing Experiments)
« on: 01/25/2023 09:33 pm »
RLV LEX-01, 02, and 03 demonstrations

See also Indian Reusable Launch Vehicle Program.



ISRO Chairman says that RLV-TD Landing Experiment (LEX) demo this week:

https://theprint.in/science/a-rocket-launcher-you-can-recycle-isro-chief-says-rlv-landing-demo-this-week/1332727/


Quote
Bhopal: The Indian Space Research Organisation (ISRO) is all set to carry out the first landing demonstration of its Reusable Launch Vehicle (RLV) Saturday, its chairperson S. Somanath has said.

Somanath, who was speaking to ThePrint on the sidelines of the 8th India International Science Festival in Bhopal, said the demonstration will continue as planned provided climate and weather conditions are suitable.

An RLV is a launch vehicle that is designed to return to the Earth substantially intact and could, therefore, be reused.

ISRO’s Reusable Launch Vehicle-Technology Demonstration (RLV-TD) Programme is a series of technology demonstration missions, seen as the first step towards realising a two-stage-to-orbit (TSTO) fully reusable vehicle. A TSTO, or a two-stage rocket, is a spacecraft in which two distinct stages provide propulsion consecutively in order to achieve orbital velocity.

This is the first time ISRO is conducting a landing demonstration for its RLV-TD Programme.


Other sources give Saturday, January 28 as the best weather date.
« Last Edit: 06/10/2024 03:48 am by sanman »

Offline zubenelgenubi

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #1 on: 02/10/2023 03:53 am »
From the post launch speeches after the successful launch of SSLV D2:
Preparing GSLV Mk.III for 36 OneWeb satellites in middle of March. Commencing launch campaign immediately after today's launch for PSLV C55 for end of March on commercial mission. Using new facility. Preparing for landing demonstration of RLV in a few days time.

For Gaganyan have abort and recovery mission today, another abort and recovery mission and trying for uncrewed mission before end of year.

GSLV for NAVIC series satellite prior to NISAR, scheduled for end of this year. More PSLV missions as well.
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Offline FutureSpaceTourist

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #3 on: 04/02/2023 04:29 am »
https://twitter.com/isro/status/1642353304339636225

Quote
India 🇮🇳 achieved it!

ISRO, joined by @DRDO_India @IAF_MCC, successfully conducted the Reusable Launch Vehicle Autonomous Landing Mission (RLV LEX)

at the Aeronautical Test Range (ATR), Chitradurga, Karnataka in the early hours on April 2, 2023.

Edit to add:

https://twitter.com/isro/status/1642377704782843905
« Last Edit: 04/02/2023 04:34 am by FutureSpaceTourist »

Offline FutureSpaceTourist

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #4 on: 04/02/2023 04:31 am »
Quote
#ISRO has conducted a drop test of their Reusable Launch Vehicle (RLV) flying test bed, culminating in a successful landing on an airstrip in Karnataka following a release at 4.5 km altitude.

This follows on from a successful hypersonic reentry test (HEX) performed in 2016.

https://twitter.com/tylerg1998/status/1642378957386313729

Quote
#ISRO is planning two more large-scale trials for their RLV-TD, including an orbital reentry test (REX) and a scramjet propulsion experiment (SPEX).

The timeline for these upcoming tests is to be determined.

Read more about RLV-TD here:

https://www.nasaspaceflight.com/2016/05/india-launch-reusable-launch-vehicle-demonstrator-mission/

Offline FutureSpaceTourist

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #5 on: 04/02/2023 05:04 am »
https://twitter.com/isro/status/1642392184333946882

Quote
RLV's autonomous approach and landing

Offline FutureSpaceTourist

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #6 on: 04/02/2023 05:32 am »
Rollout video

https://twitter.com/newsiadn/status/1642357032375447552

Quote
ISRO, DRDO, IAF Jointly Conducted RLV Test

@isro @DRDO_India and @IAF_MCC conducted the Reusable Launch Vehicle Autonomous Landing Mission (RLV LEX) successfully from Aeronautical Test Range, Chitradurga, Karnataka this morning.

Date : April 2, 2023

Offline sanman

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #7 on: 04/02/2023 05:54 am »
Youtube version of the same:



Bit of difficulty braking, given that it drifted at the end?
« Last Edit: 04/02/2023 06:01 am by sanman »

Offline sanman

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #8 on: 04/02/2023 11:01 am »
brief clip of the CH-47 Chinook carrying it

« Last Edit: 04/02/2023 11:04 am by sanman »

Offline Vahe231991

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #9 on: 04/03/2023 01:08 am »
The RLV-TD LEX reminds me of tests of the X-40 Space Maneuver Vehicle that tested the aerodynamics and navigation systems of the X-37. If the REX flights is successful, it will make India the fourth country to orbit and test a reusable spaceplane and the first country in the Global South to fly an orbital spaceplane.

Offline sanman

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #10 on: 04/03/2023 01:35 am »
So I wonder what caused the swerving at the end? My speculation is that was caused by hard braking on the nosewheel, which may have generated shimmying. While the swerving did coincide with the drogue chute release, I assume that was just a coincidence of timing, since the drogue chute release would have been immediately followed by the nosewheel braking, which is likely to have caused the swerving.

Offline sanman

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #11 on: 04/09/2023 03:39 am »
ISRO video which includes some additional footage with new camera angles:


Offline sanman

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #12 on: 04/09/2023 07:18 am »

Offline john smith 19

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #13 on: 04/09/2023 08:21 am »
The RLV-TD LEX reminds me of tests of the X-40 Space Maneuver Vehicle that tested the aerodynamics and navigation systems of the X-37. If the REX flights is successful, it will make India the fourth country to orbit and test a reusable spaceplane and the first country in the Global South to fly an orbital spaceplane.
Yup, that's exactly where they are. Of course it could be the vehicle is actually further along and all then need do now is refurb it and stick it in the nose cone of their ELV to fly it.

If that is the case then you have a slow-to-design-n-build-but-quick-to-execute programme.

Otherwise they will use the data to build a new vehicle which will be the actual spaceplane.
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Offline Michael S

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #14 on: 04/09/2023 08:40 pm »
it will make India the fourth country to orbit and test a reusable spaceplane and the first country in the Global South to fly an orbital spaceplane.

(Emphasis mine)
could you clarify what you mean by this? I'm sure I should know what you mean, but by my reckoning India is in the Northern Hemisphere.

Offline Robotbeat

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #15 on: 04/09/2023 09:40 pm »
The RLV-TD LEX reminds me of tests of the X-40 Space Maneuver Vehicle that tested the aerodynamics and navigation systems of the X-37. If the REX flights is successful, it will make India the fourth country to orbit and test a reusable spaceplane and the first country in the Global South to fly an orbital spaceplane.
Nope, China flew their spaceplane in July 2021. https://spacenews.com/china-makes-progress-in-reusability-with-secretive-second-flight-of-suborbital-spaceplane/
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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #16 on: 04/09/2023 09:45 pm »
it will make India the fourth country to orbit and test a reusable spaceplane and the first country in the Global South to fly an orbital spaceplane.

(Emphasis mine)
could you clarify what you mean by this? I'm sure I should know what you mean, but by my reckoning India is in the Northern Hemisphere.
It’s basically just a more politically correct way of saying “developing country.” Which is increasingly weird to apply to China but technically people still do. It is kind of a silly phrase to be honest. Kazakhstan, for instance, is considered “global north”
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Offline TheVarun

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #17 on: 04/09/2023 10:21 pm »
The Indian RLV was first tested in May, 2016, launched from a rocket, and landed in water( as intended).

Yes " South" refers to developing countries. Not sure China qualifies. It's essentially India, Africa, South East Asia and South America.

Offline Comga

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #18 on: 04/09/2023 10:21 pm »
it will make India the fourth country to orbit and test a reusable spaceplane and the first country in the Global South to fly an orbital spaceplane.

(Emphasis mine)
could you clarify what you mean by this? I'm sure I should know what you mean, but by my reckoning India is in the Northern Hemisphere.

The statement is of the form
(Entity) is the first (descriptor with distinctions) to achieve (some goal)

An issue is how exquisitely fine or awkward a distinction one has to make to make it be a “first”.

Do we have any information on how many of the features of an orbital and reentry vehicle the RLV-TD has beyond shape and aerodynamic controls?
What kind of wastrels would dump a perfectly good booster in the ocean after just one use?

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #19 on: 03/10/2024 04:16 pm »
https://twitter.com/ISROSpaceflight/status/1766804752636273072

Quote
The second landing experiment (LEX-02) of ISRO's Pushpak (TD) vehicle, formerly known as RLV-TD, is planned to take place before 16th March!! 🛩

The previous landing experiment - LEX-01, was conducted in April 2023. #ISRO

Picture of the vehicle to be used on LEX-02
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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #20 on: 03/22/2024 08:13 am »
https://twitter.com/ISROSpaceflight/status/1771092790820082028
Quote
RLV LEX-02 Mission Accomplished! 🎯

Today at 7:10 am, an IAF Chinook dropped #Pushpak from an altitude of 4.5 km & 4 km dist. from runway.

Pushpak autonomously made turns to align itself as it glided down & successfully touched down on the runway! #ISRO
« Last Edit: 03/22/2024 06:12 pm by zubenelgenubi »
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Offline ethan829

Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #21 on: 03/22/2024 10:24 am »

Offline FutureSpaceTourist

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #22 on: 03/22/2024 03:11 pm »

Offline sanman

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #23 on: 03/22/2024 05:01 pm »

Offline catdlr

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Re: RLV-TD LEX-01 and -02 (Landing Experiments)
« Reply #24 on: 03/22/2024 07:31 pm »
Just some added video not in the cut post above

https://twitter.com/ISROSpaceflight/status/1771138156785770687

Quote
Full video of RLV-TD aka #Pushpak LEX-02 from airlift to drop from an IAF Chinook helicopter followed by landing! 🚁 #ISRO
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Offline sanman

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Re: RLV-TD LEX-01, -02 and -03 (Landing Experiments)
« Reply #26 on: 06/10/2024 03:48 am »
LEX-03 flight coming up, according to this NOTAM:

Quote
A1649/24 - GPS RADIO SONDE BALLOON ASCENTS WILL TAKE PLACE FM
AERONAUTICAL TEST RANGE, VARAVINA KAVAL, CHITRADURGA,
AS PER THE FLW DETAILS.
LAUNCH SITE: AERONAUTICAL TEST RANGE, VARAVINA KAVAL,
CHITRADURGA, 142313N 0763337E.
BALLOON COLOUR: WHITE.
WT: 600 GRAMS.
BALLOON DIAMETER AFTER HELIUM GAS FILLING: 2M.
PAYLOAD WT: 125 GRAMS.
THREAD LEN: 15M.
BALLOON HGT: UP TO 30 KM.
BALLOON ASCENT RATE: 5MPS OR 18 KMH.
BALLOON ASCENT DUR: 01HR 20MIN.
BALLOON DESCENT RATE: 15 TO 20MPS.
BALLOON TRANSMITTING FREQ: 400MHZ TO 406MHZ.
BALLOON LAUNCH WILL TAKE PLACE AT 2330 0100 AND 0230.
LAST BALLOON TOUCHDOWN BEFORE 0430. GND - UNL, BTN 2330-0430, 28 MAY 23:30 2024
UNTIL 14 JUN 04:30 2024
. CREATED: 28 MAY 11:05 2024

This 3rd and final landing experiment should happen in the next 4 days
« Last Edit: 06/10/2024 04:17 am by sanman »

Offline sanman

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Re: RLV-TD LEX-01, -02 and -03 (Landing Experiments)
« Reply #27 on: 06/10/2024 03:53 am »
https://www.thehindu.com/sci-tech/science/isro-all-set-for-third-reusable-launch-vehicle-landing-experiment/article68266926.ece

Quote
ISRO All Set for Third Reusable Launch Vehicle Landing Experiment

...
RLV-LEX missions involve taking an unmanned winged prototype, christened Pushpak, to a designated height and releasing it to land safely under varying conditions. In LEX-03, Pushpak will be carried to a height of 4.5 km and 500 metres to one side of the runway using an IAF Chinook helicopter and released. In LEX-02, the second mission, the altitude was the same but the lateral distance from the runway was 150 metres.

“It has to autonomously approach the runway, manoeuvre by making crossrange, downrange and altitude corrections to touch down on the runway,” he said. The LEX-03 mission will look at how the sink rate, or the rate of descent, can be cut down to reduce the impact load. It will also have on board a real-time kinematics (RTK) package. Yet another challenge before the upcoming mission is handling tailwind conditions.
...
In the next stage of tests under the RLV-TD, the ISRO will use an unmanned Orbital Re-entry Vehicle (ORV). The vehicle used will be 1.6 times the size of ‘Pushpak’‘ used for LEX. It will be placed in a 400 km orbit around earth using a modified Geosynchronous Satellite Launch Vehicle (GSLV). This mission is expected in two years time. “Various experiments will be carried out in orbit. It will have, among other things, a thermal protection system for safe re-entry into the earth’s atmosphere and a retractable landing gear. The ISRO has started work on the ORV,” Dr. Unnikrishnan Nair said.
...
« Last Edit: 06/10/2024 04:04 am by sanman »

Offline FutureSpaceTourist

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Re: RLV-TD LEX-01, -02 and -03 (Landing Experiments)
« Reply #28 on: 06/14/2024 06:41 am »
https://twitter.com/chethan_dash/status/1801489495830773987

Quote
#Update #space

Weather permitting, @isro will attempt the #RLV 3rd landing experiment (#RLVLEX3) as early as next week. And, “issues” with the chopper are delaying #IADT (integrated air-drop test) part of #Gaganyaan. RLV test in Challakere, Karnataka, IADT in Sriharikota. 1/n

Isro, which had  completed #RLVLEX02 on March 22, is gearing up for LEX3, which will build upon LEX-02 aimed at improving the vehicle’s performance, guidance, and landing capabilities. 2/n

“We are waiting. The helicopter is there but weather is bad. It is expected to improve by 14th & if that happens we can conduct the experiment next week. This'll be the last landing experiment. Next, we’ll attempt orbital re-entry,” VSSC director S Unnikrishnan Nair told me. 3/n

Compared to the previous LEX, Nair said, #RLVLEX3 will be more challenging as the “intentional cross-range error of around 500m will be tested, compared to around 150m during LEX2. 4/n

“The velocity azimuth with respect to the runway centre has been adjusted to 2°, deviating from the previous mission's 0° alignment,” he said. 5/n

The mission will have another advancement: Implementation of advanced guidance algorithm that can simultaneously correct errors in both longitudinal & lateral planes. This decoupled algorithm, improvement over LEX02’s approach, will be utilised to enhance precision & control. 6/n

Also, to ensure a softer landing and reduce touchdown loads, the main landing gear (MLG) sink rate has been reduced to less than 1m/second, compared to the 1.5m/second limit during LEX2. 7/n

Additionally, a smoke marker system has been introduced to trace the descent trajectory, providing visual data for analysis and future improvements. Isro will also evaluate the performance of its real-time kinematics (RTK) system in a high-speed environment. 8/n

This system is crucial for future landing missions, as it can enhance the robustness of the hybrid navigation system, ensuring accurate and reliable guidance. 9/n

On the other hand, #IADT of a simulated crew module to validate the parachute system for #Gaganyaan, has been put on hold as need to revisit “some aspects” of the helicopter (Chinook) selected to carry out the test, arose. 10/n

During the test, crew module, weighing around 3tonne, will be dropped from the Chinook at an altitude of 3km, & a sequence of parachute deployments will occur before splashdown & recovery. Proposed IADT is part of several such tests to be part of Gaganyaan’s preparations. 11/n

I had reported in May that pre-mission trials had begun for this. “...During the pre-mission trials for the first IADT in Sriharikota, it was noticed that the helicopter may have ‘some issues’ that needed to be addressed. That is progressing now,” a source said. 12/n

IAF, whose helicopter Isro is using for the mission, is conducting an investigation “to understand what needs to be done”, the source said, adding that Isro was waiting for IAF to get back with its findings before moving ahead. 13/n

Isro plans to conduct 7 IADTs as per initial plans, with final number depending on test results. Alongside these, it's preparing for at least 1 uncrewed mission & the second test vehicle mission to test various abort conditions as part of #Gaganyaan this year. n/n

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Re: RLV-TD LEX-01, -02 and -03 (Landing Experiments)
« Reply #29 on: 06/23/2024 05:21 am »
https://twitter.com/isro/status/1804695916617863425

Quote
Hat-trick for ISRO in RLV LEX! 🚀

🇮🇳ISRO achieved its third and final consecutive success in the Reusable Launch Vehicle (RLV) Landing EXperiment (LEX) on June 23, 2024.

"Pushpak" executed a precise horizontal landing, showcasing advanced autonomous capabilities under challenging conditions.

With the objectives of RLV LEX accomplished, ISRO embarks into RLV-ORV, the orbital reusable vehicle.

@IAF_MCC @DRDO_India @CSIRNALOFFICIAL
@IITKanpur @IndianOilcl @AAI_Official

Quote
RLV-LEX3 images

https://twitter.com/isro/status/1804709607576834363

Quote
RLV-LEX3 Video


Quote
June 23, 2024
ISRO completes its RLV technology demonstrations through LEX trio

The Indian Space Research Organisation (ISRO) has proudly achieved a third consecutive success in the Reusable Launch Vehicle (RLV) Landing EXperiment (LEX) on June 23, 2024. The third and final test in the series of LEX (03) was conducted at 07:10 IST at the Aeronautical Test Range (ATR) in Chitradurga, Karnataka.

Following the success of the RV LEX-01 and LEX-02 missions, RLV LEX-03 re-demonstrated the autonomous landing capability of the RV under more challenging release conditions (cross range of 500 m against 150 m for LEX-02) and more severe wind conditions. The winged vehicle, named 'Pushpak', was released from an Indian Air Force Chinook Helicopter at an altitude of 4.5 km. From a release point 4.5 km away from the runway, Pushpak autonomously executed cross-range correction manoeuvres, approached the runway and performed a precise horizontal landing at the runway centreline. Due to this vehicle's low lift-to-drag ratio aerodynamic configuration, the landing velocity exceeded 320 kmph, compared to 260 kmph for a commercial aircraft and 280 kmph for a typical fighter aircraft. After touchdown, the vehicle velocity was reduced to nearly 100 kmph using its brake parachute, after which the landing gear brakes were employed for deceleration and stop on the runway. During this ground roll phase, Pushpak utilises its rudder and nose wheel steering system to autonomously maintain a stable and precise ground roll along the runway.

This mission simulated the approach and landing interface and high-speed landing conditions for a vehicle returning from space, reaffirming ISRO's expertise in acquiring the most critical technologies required for the development of a Reusable Launch Vehicle (RLV). Through this mission, the advanced guidance algorithm catering to longitudinal and lateral plane error corrections, which is essential for the future Orbital Re-entry Mission has been validated. The RLV-LEX uses multisensor fusion including sensors like Inertial sensor, Radar altimeter, Flush air data system, Pseudolite system and NavIC. Notably, the RLV-LEX-03 mission reused the winged body and flight systems as such without any modification, from the LEX-02 mission, demonstrating the robustness of ISRO's capability of design to reuse flight systems for multiple missions.

This mission simulates the approach & landing interface and high-speed landing conditions for a vehicle returning from space, which will reaffirm ISRO's expertise in acquiring the most critical technologies required for the development of a Reusable Launch Vehicle (RLV).

The mission, led by VSSC, was a collaborative effort involving multiple ISRO centres SAC, ISTRAC, SDSC-SHAR, with significant support from the Indian Air Force (IAF), Aeronautical Development
Certification (CEMILAC), National Aerospace Laboratories (NAL), Indian Institute of Technology, Kanpur, Indian aerospace industrial partners, Indian Oil Corporation of India and Airport Authority of
Director of VSSC, emphasised that this consistent success boosts ISRO's confidence in the critical technologies essential for future orbital re-entry missions.

Shri. J Muthupandian is the Mission Director and Shri. B Karthik is the Vehicle Director for this successful mission.
« Last Edit: 06/23/2024 05:22 am by FutureSpaceTourist »

Offline FutureSpaceTourist

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Re: RLV-TD LEX-01, -02 and -03 (Landing Experiments)
« Reply #30 on: 06/23/2024 05:43 am »
https://twitter.com/chethan_dash/status/1804698007364858166

Quote
#JUSTIN #Space #Update

@isro, which on March 22 did the 2nd landing experiment of reusable launch vehicle (#RLV) — “#RLVLEX02” — today conducted the 3rd & last landing test (#RLVLEX03), paving the way for an orbital re-entry test. 1/n

Pic: Isro (from lex2). New pics awaited

The test was conducted at 7.10am at the Aeronautical Test Range (ATR) at Challakere in Chitradurga district, some 220km from Bengaluru. 2/n

The RLV project is an important programme that will demonstrate one of the technologies needed to meet India’s ambitions of sustained human presence in space. 3/n

The RLV-LEX-03, built upon RLV-LEX-02, was aimed at improving the vehicle’s performance, guidance, and landing capabilities. I’d reported last week that, weather permitting, Isro would attempt to achieve this milestone in the development of RLV technology this week. 4/n

VSSC director S Unnikrishnan Nair had told me that compared to LEX02, LEX3 will be more challenging as the “intentional cross-range error of around 500m will be tested, compared to around 150m during LEX02.  5/n

On Sunday, Isro said: “LEX03 re-demonstrated the autonomous landing capability of the RLV under more challenging release conditions (cross range of 500m) & more severe wind conditions. RLV, named 'Pushpak, was released from an IAF Chinook helicopter at an altitude of 4.5km.” 6/n

From a release point, the vehicle autonomously executed cross-range correction manoeuvres, approached the runway and performed a precise horizontal landing at the runway centreline. 7/n

“Due to its low lift-to-drag ratio aerodynamic configuration, the landing velocity exceeded 320kmph, compared to 260kmph for a commercial aircraft and 280 kmph for a typical fighter aircraft.,” Isro said. 8/n

After touchdown, the vehicle velocity was reduced to nearly 100kmph using its brake parachute, after which the landing gear brakes were employed for deceleration and stop on the runway. 9/n

“During this ground roll phase, the vehicle utilised its rudder and nose wheel steering system to autonomously maintain a stable and precise ground roll along the runway, Isro said. 10/n

It added that the mission simulated the approach and landing interface and high-speed landing conditions for a vehicle returning from space,” Isro said. 11/n

The mission had another advancement: Implementation of an advanced guidance algorithm that can simultaneously correct errors in both the longitudinal and lateral planes — essential for the future orbital re-entry mission. 12/n

This decoupled algorithm, an improvement over LEX-02’s approach, will be utilised to enhance the reusable launch vehicle’s precision and control. 13/n

“The RLV-LEX uses multisensor fusion including sensors like inertial sensor, radar altimeter, flush air data system, pseudolite system and NaviC… 14/n

…Notably, the mission reused the winged body and flight systems as such without any modification, from the LEX-02 mission, demonstrating the robustness of Isro’s capability of design to reuse flight systems for multiple missions,” Isro said. 15/n

This mission simulated the approach & landing interface and high-speed landing conditions for a vehicle returning from space, which will reaffirm Isro’s expertise in acquiring the most critical technologies required for the development of an RLV. n/n

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Re: RLV-TD LEX-01, -02 and -03 (Landing Experiments)
« Reply #31 on: 06/23/2024 06:07 am »

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Re: RLV-TD LEX-01, -02 and -03 (Landing Experiments)
« Reply #32 on: 06/26/2024 01:35 pm »
https://twitter.com/chethan_dash/status/1805918663226048520

Quote
#Space #Update

With 3rd & final landing experiment having been completed on June 23, #RLV will go through several modifications to qualify for the planned Orbital Re-entry Test/Flight. 1/n

Read on for details. Also Watch: shorturl.at/2Fgjr

The orbital re-entry demonstration will involve vertical launching of #RLV into space and bringing it back safely to land on a runway. Isro may need to carry out multiple orbital re-entry tests and RLV will be 6 times the size of the #RLVTD. 2/n

The GSLV that will carry the scaled-up RLV, expected to weigh around 3.5 tonne to 4 tonne, to space will forego its cryogenic upper stage (CUS), which will be replaced by a rejigged version of the PS4 — the last stage of #PSLV. 3/n

S Unnikrishnan Nair, director, VSSC told me: “Although overall size will increase, increase in mass won’t increase six times. Therefore, given the weight of the vehicle, we wouldn’t need the energy the GSLV can produce with the cryo stage, that’s why we are using the PS4.” 4/n

The scaled-up RLV would also have enhanced thermal protection, which is crucial to prevent burning up of the vehicle during the re-entry phase. “Take off and landing are very critical for any aircraft… 5/n

…For us, take off will be vertical. For landing to be smooth, we’ll have to work on various systems that enable re-entry, approaching runway, touching correct place & aligning with centre line, deployment of parachutes etc. Software will have to be written too,” Nair said. 6/n

During re-entry, the belly of the vehicle needs to be shown to increase the drag and reduce the speed — that is, energy manoeuvring from orbit to touchdown. 7/n

Aside from modifications of thermal protection systems, enhanced software and NGC (navigation, guidance and control) and other sub-systems, the vehicle will need a different landing gear. 8/n

For the prototype (RLV-TD), Isro had used a fixed landing gear supplied by Bengaluru-based Timetooth Technologies, which will have to be replaced by a deployable one. 9/n

And, Timetooth, which has supplied around five fixed landing gear systems for the programme so far, is optimistic of bagging the new order as well. 10/n

The firm’s co-founder, Girish Mudgal, said: “We’re very optimistic. We’ve been working on a retractable version of the landing gear… 11/n

…We don’t know Isro’s exact plans for the orbital re-entry version, but we’ve built an extreme amount of trust and reputation for Isro to see us as a reliable partner for this programme.” 12/n

Other than Isro, Timetooth has supplied landing gears to DRDO as well. “...As far as we’re aware, we are India’s only company which has worked on the long endurance or large drones landing systems… 13/n

…We supplied our system for DRDO’s Rustom (now Tapas) drone, which had its maiden flight in 2016. And after that, there have been about over 200 flights,” Mudgal said. 14/n

Besides, Isro will also need to look for a larger runway to accommodate the landing of the orbital re-entry vehicle. And initially, it will have to rely on the Indian Air Force (IAF) to find a suitable runway. 15/n

“The landing site will have to be decided as it cannot happen in Chitradurga. We need a location that allows us to fly mostly over sea & requires minimal flying over land and populated areas. Flight over landmass must be minimal. We’ll have to discuss it with IAF,” Nair said. n/n

Tags: India lex rex spaceplane 
 

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