- Space Technology
- Space Technology Unit 1
- Orbit
- Launchers or Launch Vehicles
- Evolution of Indian Launch Vehicles
- Key Indian space organizations
- Indian Space Research Organisation (ISRO)
- Vikram Sarabhai Space Centre
- Liquid Propulsion Systems Centre (LPSC)
- Satish Dhawan Space Centre (SDSC)
- U R Rao Satellite Centre (URSC),
- Space Applications Centre (SAC)
- National Remote Sensing Centre (NRSC)
- Human Space Flight Centre (HSFC)
- ISRO Propulsion Complex (IPRC)
- ISRO Inertial Systems Unit (IISU)
- ISRO Telemetry, Tracking and Command Network (ISTRAC)
- Master Control Facility (MCF)
- Laboratory for Electro-Optics Systems (LEOS)
- Indian Institute of Remote Sensing (IIRS)
- Indian Space Research Organisation (ISRO)
- Space Sector Reforms and Private Participation
- Indian space Policy, 2023
- Indian National Space Promotion and Authorization Center (IN-SPACe)
- Antrix Corporation Limited
- NewSpace India Limited (NSIL)
- Private sector in Space Technology
- Mission Prarambh & India’s First Private Launch Vehicle: Vikram-S
- Agnikul Cosmos and the Agnibaan SOrTeD Mission
- Other initiatives of ISRO
- PM Modi “directs” ISRO to land man on moon by 2040
- Anti-Satellite Missile Test (ASAT) – Mission Shakti
- YUVIKA – YUva VIgyani KAryakram (Young Scientist Programme)
- NEtwork for space object TRacking and Analysis (NETRA)
- Indian Space Missions and Applications
- Space Based Earth Observation Applications
- Important Foreign Missions
- Recent Missions
- PREVIOUS YEAR QUESTIONS – Space Technology
- MAINS PREVIOUS YEAR QUESTIONS – Space Technology
- GLOSSARY
Human rated LVM3 - HLVM3
- LVM3 rocket – The well proven and reliable heavy lift launcher of ISRO, is identified as the launch vehicle for Gaganyaan mission. It consists of solid stage, liquid stage and cryogenic stage. All systems in LVM3 launch vehicle are re-configured to meet human rating requirements and christened Human Rated LVM3. HLVM3 will be capable of launching the Orbital Module to an intended Low Earth Orbit of 400 km.
- HLVM3 consists of Crew Escape System (CES) powered by a set of quick acting, high burn rate solid motors which ensures that Crew Module along with crew is taken to a safe distance in case of any emergency either at launch pad or during ascent phase.