User talk:JugrajSingh1

Chandrayan-3
Chandrayaan-3 is a follow-on mission to Chandrayaan-2 to demonstrate end-to-end capability in safe landing and roving on the lunar surface. It consists of Lander and Rover configuration. It will be launched by LVM3 from SDSC SHAR, Sriharikota. The propulsion module will carry the lander and rover configuration till 100 km lunar orbit. The propulsion module has Spectro-polarimetry of Habitable Planet Earth (SHAPE) payload to study the spectral and Polari metric measurements of Earth from the lunar orbit. Lander payloads: Chandra’s Surface Thermophysical Experiment (ChaSTE) to measure the thermal conductivity and temperature; Instrument for Lunar Seismic Activity (ILSA) for measuring the seismicity around the landing site; Langmuir Probe (LP) to estimate the plasma density and its variations. A passive Laser Retroreflector Array from NASA is accommodated for lunar laser ranging studies. Rover payloads: Alpha Particle X-ray Spectrometer (APXS) and Laser Induced Breakdown Spectroscope (LIBS) for deriving the elemental composition in the vicinity of landing site. More Details

Chandrayaan-3 consists of an indigenous Lander module (LM), Propulsion module (PM) and a Rover with an objective of developing and demonstrating new technologies required for Inter planetary missions. The Lander will have the capability to soft land at a specified lunar site and deploy the Rover which will carry out in-situ chemical analysis of the lunar surface during the course of its mobility. The Lander and the Rover have scientific payloads to carry out experiments on the lunar surface. The main function of PM is to carry the LM from launch vehicle injection till final lunar 100 km circular polar orbit and separate the LM from PM. Apart from this, the Propulsion Module also has one scientific payload as a value addition which will be operated post separation of Lander Module. The launcher identified for Chandrayaan-3 is GSLV-Mk3 which will place the integrated module in an Elliptic Parking Orbit (EPO) of size ~170 x 36500 km. The mission objectives of Chandrayaan-3 are: To demonstrate Safe and Soft Landing on Lunar Surface To demonstrate Rover roving on the moon and To conduct in-situ scientific experiments. To achieve the mission objectives, several advanced technologies are present in Lander such as, Altimeters: Laser & RF based Altimeters Velocimeters: Laser Doppler Velocimeter & Lander Horizontal Velocity Camera Inertial Measurement: Laser Gyro based Inertial referencing and Accelerometer package Propulsion System: 800N Throttleable Liquid Engines, 58N attitude thrusters & Throttleable Engine Control Electronics Navigation, Guidance & Control (NGC): Powered Descent Trajectory design and associate software elements Hazard Detection and Avoidance: Lander Hazard Detection & Avoidance Camera and Processing Algorithm Landing Leg Mechanism. To demonstrate the above said advanced technologies in earth condition, several Lander special tests have been planned and carried out successfully viz. Integrated Cold Test - For the demonstration of Integrated Sensors & Navigation performance test using helicopter as test platform Integrated Hot test – For the demonstration of closed loop performance test with sensors, actuators and NGC using Tower crane as test platform Lander Leg mechanism performance test on a lunar simulant test bed simulating different touch down conditions. JugrajSingh1 (talk) 10:03, 20 August 2023 (UTC)

Speedy deletion nomination of User:JugrajSingh1


A tag has been placed on User:JugrajSingh1, requesting that it be deleted from Wikipedia. This has been done under two or more of the criteria for speedy deletion, by which pages can be deleted at any time, without discussion. If the page meets any of these strictly defined criteria, then it may soon be deleted by an administrator. The reasons it has been tagged are:
 * It appears to be an unambiguous copyright infringement of https://www.indiastrategic.in/count-down-begins-for-the-much-anticipated-chandrayaan-3-mission/. (See section G12 of the criteria for speedy deletion.) For legal reasons, we cannot accept copyrighted text or images taken from other web sites or printed material, and as a consequence, your addition will most likely be deleted. You may use external websites or other printed material as a source of information, but not as a source of sentences. This part is crucial: say it in your own words. Wikipedia takes copyright violations very seriously and persistent violators will be blocked from editing.If the external website or image belongs to you, and you want to allow Wikipedia to use the text or image — which means allowing other people to use it for any reason — then you must verify that externally by one of the processes explained at Donating copyrighted materials. The same holds if you are not the owner but have their permission. If you are not the owner and do not have permission, see Requesting copyright permission for how you may obtain it. You might want to look at Wikipedia's copyright policy for more details, or ask a question here.
 * It appears to consist of writings, information, discussions, and/or activities not closely related to Wikipedia's goals. Please note that Wikipedia is not a free Web hosting service. (See section U5 of the criteria for speedy deletion.)

If you think this page should not be deleted for this reason, you may contest the nomination by visiting the page and clicking the button labelled "Contest this speedy deletion". This will give you the opportunity to explain why you believe the page should not be deleted. However, be aware that once a page is tagged for speedy deletion, it may be deleted without delay. Please do not remove the speedy deletion tag from the page yourself, but do not hesitate to add information in line with Wikipedia's policies and guidelines. Schminnte (talk • contribs) 20:15, 20 August 2023 (UTC)