Chandrayaan-3

Chandrayaan-3 Lunar Landing Success Prediction

@kaggle.shahidulugvcse_chandrayaan_3

Propulsion Module

@kaggle.shahidulugvcse_chandrayaan_3.propulsion_module

parameter Parameter	specifications Specifications
Lunar Polar Orbit	From 170 x 36500 km to lunar polar orbit
Mission life	Carrying Lander Module & Rover upto ~100 x 100 km launch injection. Subsequently, operation of experimental payload for a period of 3 to 6 months.
Structure	Modified version of I-3 K
Dry Mass	448.62 kg (including pressurant)
Propellant Mass	1696.39 kg
Total PM Mass	2145.01 kg
Power Generation	738 W, Summer solistices and with bias
Communication	S-Band Transponder (TTC) – with IDSN
Attitude Sensors	CASS, IRAP, Micro star sensor
Propulsion System	Bi-Propellant Propulsion System (MMH + MON3)


CREATE TABLE propulsion_module (
  "parameter" VARCHAR,
  "specifications" VARCHAR
);