INDIAN SPACE COMMAND X PROJECT VAYUSPACE
๐ฎ๐ณ Indian Space Command ร Project Vayuspace Lunar Propulsion Module + Lander Mission The mission consists of a Propulsion Module (PM) and a Lander Module (LM). The PM carries the lander toward lunar orbit, then the two modules separate so the lander can perform its descent and landing. This is similar in overall mission architecture to Chandrayaan-3. ๏ฟฝ ISRO +1 Project Vayuspace Lander: ๐ฌ A dedicated lunar lander designed for the SFS mission ๐ฆฟ Landing legs for touchdown ๐ฅ Descent engines for lunar landing โ๏ธ Solar power ๐ก Communications and navigation systems ๐ Docking interface with the Propulsion Module Mission: ๐ Launch โ ๐ Earth orbit โ ๐ Lunar transfer โ ๐ฐ๏ธ Lunar orbit โ ๐ PM/LM separation โ ๐ฌ Vayuspace Lander landing
Blueprint facts
| Difficulty | Medium |
|---|
Requirements
- Difficulty: medium.
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