==Future Mission==
Small satellite launch vehicle - SSLV
Reusable Launch vehicle
ISS
Gaganyan
==On going Mission==
GSLV-F14/INSAT-3DS - February 17, 2024
PSLV-C58 / [[XPoSat]] Mission
Aditya L1 PSLV-C57/Aditya-L1 Mission
Chandrayan 3
Quantum Plan
LOX Methane
==Future Aim==
Indian Space Station to be set up by 2035
India to send Man to Moon by 2040
India to undertake missions to Venus and Mars
==Small Satellite Launch Vehicle - SSLV==
- 3 solid propulsion stages
- Velocity Trimming Model - VTM - Fluid Propulsion
![[1000043996.png]]
==Reusable Launch Vehicle - RLV==
-
2016 - Hypersonic Flight Experiment -HEX - 5x sound speed ( speed of sound 343 m / s)
-
2023 - Autonomous RLV Landing Experiment
- The Reusable Launch Vehicle (RLV) named ==Pushpak== was designed for complex maneuvers and autonomous landings. An Indian Airforce Chinook helicopter lifted Pushpak to 4.5 km altitude and released it 4 km from the runway. Pushpak then autonomously flew to the runway, made necessary adjustments, and landed precisely using its brake parachute, landing gear brakes, and nose wheel steering.
- 📍Aeronautical Test Range (ATR), Chitradurga in Karnataka, April 2,2023
![[1000043999.jpg]]
- Similar experiment conducted on 2016
- RLV TD 1 : 65km high, 5x sound speed, 450km travel, droped in Bay of Bengal, near by sriharikota.
-
Future test : Orbital Re-entry Experiment - ORE
==ISS or Bharatiya Antariksha Station==
In 2019, ISRO chief K. Sivan presented the features of the proposed space station for the first time.
2024 3rd quarter: Space Docking Experiment - SPADEX
==Gaganyaan==
Gaganyaan project envisages demonstration of human spaceflight capability by launching crew of 3 members to an orbit of 400 km for a 3 days mission and bring them back safely to earth, by landing in Indian sea waters.
- Integrated Air Drop Test - IADT
- Pad Abort Test - PAT
- Test Vehicle - TV
- Gaganyan Experimental Mission - G-X
- G1 & G2 before H1
Human Rated Launch Vehicle - HLV M3 includes Crew Module CM, Service Module SM, Orbital Module OM.
HLV M3 will be capable of launching the Orbital Module to an intended Low Earth Orbit of 400 km.
![[1000044003.jpg]]
Astronaut Designates - ADs
![[1000044004.jpg]]
Training at Astronaut Training Facility ATF , Bangalore
Gaganyaan TV-D1 Mission, Oct 21, 2023
In-flight Abort Demonstration of Crew Escape System (CES)” at Mach number 1.2 with the newly developed Test Vehicle followed by Crew Module separation & safe recovery.
- Mach number: ratio of flow velocity past a boundary to the local speed of sound. It is named after the Czech physicist and philosopher Ernst Mach.
Ongoing Mission
GSLV-F14/INSAT-3DS MISSION
February 17,2024,from Sriharikota.
Mission: Meteorological services Data relay and Satellite Aided Search & Rescue services
Payloads: 6 channel Imager19 channel SounderData Relay Transponder (DRT)Satellite Aided Search & Rescue transponder (SAS&R)
Orbit: Geostationary orbit
GSLV-F14
Geosynchronous Satellite Launch Vehicle (GSLV) is a three-stage 51.7 m long launch vehicle having a liftoff mass of 420 tonnes.
INSAT-3DS
Third Generation Meteorological Satellite from Geostationary Orbit.The satellite will augment the Meteorological services along with the presently operational INSAT-3D and INSAT-3DR satellites
PSLV-C58 / XPoSat Mission
January 01,2024
PSLV - C58
XPoSat - X-ray Polarimeter Satellite
Mission: The first dedicated scientific satellite from ISRO to carry out research in space-based polarisation measurements of X-ray emission from celestial sources.
Payloads: POLIX (Polarimeter Instrument in X-rays) and XSPECT (X-ray Spectroscopy and Timing). POLIX is realized by Raman Research Institute and XSPECT is by Space Astronomy Group of URSC.
Orbit: Eastward low inclination orbit
![[1000044008.jpg]]
![[1000044010.jpg]]
![[1000044011.jpg]]
PSLV-C57/Aditya-L1 Mission
Sep 2,2023:launch of Aditya-L1 by PSLV-C57
Jan 6, 2024 : Halo-Orbit Insertion (HOI)
Aditya L1 shall be the first space based Indian mission to study the Sun.
The spacecraft shall be placed in a halo orbit around the Lagrange point 1 (L1) of the Sun-Earth system, which is about 1.5 million km from the Earth.
L1 point has the major advantage of continuously viewing the Sun without any occultation/eclipses
This will provide a greater advantage of observing the solar activities and its effect on space weather in real time.
The spacecraft carries seven payloads to observe the photosphere, chromosphere and the outermost layers of the Sun (the corona) using electromagnetic and particle and magnetic field detectors.
Payloads made by Indian Institute of Astrophysics IIA - Bangalore and Inter University Centre for Astronomy and Astrophysics - IUCAA - Pune
Lagrange Points are positions in space where the gravitational forces of a two-body system like the Sun and Earth produce enhanced regions of attraction and repulsion. These can be used by spacecraft as “parking spots” in space to remain in a fixed position with minimal fuel consumption.
![[1000044005.jpg]]
L1 - Aditya, L2 - James Webb
![[1000044006.jpg]]
Chandrayan III
Launched on 14th July 2023
https://x.com/narendramodi/status/1679728845149052930?t=ZJlPNDpctnWTq75HTE9arA&s=19
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 launched by LVM3 from SDSC SHAR, Sriharikota.
Mission
- To demonstrate Safe and Soft Landing on Lunar Surface
- To demonstrate Rover roving on the moon
- To conduct in-situ scientific experiments
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.
In lander Payloads: A passive Laser Retroreflector Array from NASA is accommodated for lunar laser ranging studies.
![[1000044007.webp]]
Russia
https://x.com/isro/status/1689845612865523713?t=0sVATSeChx0WCyQywCDGMg&s=19
August 12, Dr. Vikram A Sarabhai
https://x.com/isro/status/1690185902763446272?t=OTmvi-KpFT0aVUU4euGQ1g&s=19
August 21
https://x.com/isro/status/1693549487653048418?t=QC020O2fHbLCz3pZWt_KVQ&s=19
August 23, 2023
Mission 1: safe and soft landing
https://x.com/isro/status/1694327198394863911?t=vG6cmX_wIu_VqLgWxMykHA&s=19
Shiv Shakti is located at the coordinates 69.373°S 32.319°E and lies between the lunar craters Manzinus C and Simpelius N
https://x.com/PMOIndia/status/1695265187094241416?t=uXYLj5Sz8URB1G9BFVg_lg&s=19
Tiranga is located on the coordinates 70.8810°S 22.7840°E and it lies between Manzinus C and Simpelius N craters.
https://x.com/PMOIndia/status/1695266757684904037?t=s3b7g3py6K0h9nKoY1HM7Q&s=19
National Space Day
https://x.com/PMOIndia/status/1695269172534501592?t=XxAJ_SQQcN01uJ9CJOKDJg&s=19
Mission 2 : Rover Roving
![[1000044012.jpg]]
The ‘
image of the mission’ was taken by the Navigation Camera onboard the Rover (NavCam).
NavCams for the Chandrayaan-3 Mission are developed by the Laboratory for Electro-Optics Systems (LEOS)
Sep 2 , 2023
https://x.com/isro/status/1697874341604835828?t=Oler7Cq6hLDYYvURPiIBqw&s=19
In-situ scientific experiments
Mission 3 :
Instrument for the Lunar Seismic Activity (ILSA) payload on Chandrayaan 3 Lander — the first Micro Electro Mechanical Systems (MEMS) technology-based instrument on the moon — has recorded the movements of Rover and other payloads.
Additionally, it has recorded an event, appearing to be a natural one, on August 26, 2023. The source of this event is under investigation.
ILSA payload is designed and realised LEOS, Bangalore. The deployment mechanism is developed by URSC, Bengaluru.
29 , Aug
Laser-Induced Breakdown Spectroscope (LIBS) instrument onboard the Rover unambiguously confirms the presence of
Sulphur (S) in the lunar surface near the south pole, through first-ever in-situ measurements.
Al, Ca, Fe, Cr, Ti, Mn, Si, and O are also detected, as expected. Search for Hydrogen (H) is underway.
LIBS instrument is developed at the
Laboratory for Electro-Optics Systems (LEOS)/ISRO, Bengaluru.
Another instrument The Alpha Particle X-ray Spectroscope (APXS) has detected S.
Aug 31
Radio Anatomy of Moon Bound Hypersensitive Ionosphere and Atmosphere - Langmuir Probe (RAMBHA-LP) payload onboard Chandrayaan-3
The initial assessment indicates that the plasma near the lunar surface is relatively sparse.
These quantitative measurements potentially assist in mitigating the noise that Lunar plasma introduces into radio wave communication. Also, they could contribute to the enhanced designs for upcoming lunar visitors.
RAMBHA-LP payload development is led by SPL/VSSC, Thiruvananthapuram.
Hop Experiment , Sep 4
https://x.com/isro/status/1698570774385205621?t=kT4grTgaRgzoZihWqvQ63w&s=19
Sleep Sep 4
https://x.com/isro/status/1698618694795219401?t=53Ydcgt0X5cUj0bY9csRuQ&s=19
Japan entry
https://x.com/isro/status/1699640970017747332?t=fa4fqTShbgeUNYXpaZcNUA&s=19
October 17 meeting
https://x.com/isro/status/1714269764070359431?t=rVKMGGgv8sz-bQY40hEnNQ&s=19
ISRO makes breakthrough demonstration of free-space Quantum Key Distribution (QKD) over 300 m
A number of key technologies were developed indigenously to accomplish this major feat, which included the use of indigenously developed NAVIC receiver for time synchronization between the transmitter and receiver modules, and gimbal mechanism systems instead of bulky large-aperture telescopes for optical alignment.
The demonstration has included live videoconferencing using quantum-key-encrypted signals. This is a major milestone achievement for unconditionally secured satellite data communication using quantum technologies.
LOX Methane
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