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Economic and Performance Analysis of Indian Space Transportation Systems
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Economic and Performance Analysis of Indian Space Transportation Systems
AIAA SPACE 2010 ConferenceAnaheim, CA
ByPrasad Sundararajan
August 31, 2010
Economic and Performance Analysis of Indian Space Transportation Systems
Indian Space Program (ISP) Application Oriented - Telecom, Remote Sensing, Meteorology Strategic Framework – Space Policy Goals Autonomy in access to SPACE
Evolution of Indian Space Transportation Systems (STS) Sounding Rockets – Atmospheric Research SLV-3 and ASLV – Reaching the LEO PSLV – SSO and Beyond
– Space Capsule Recovery Experiment: SRE 1 (2007) & SRE 2 (2010) GSLV – GTO and Planetary Exploration Human Spaceflight Program – first mission by 2015-16 Planetary Exploration
– Future Missions to Mars (2014), Asteroids/ Comets (2016) and Outer Solar System (2018+)
Indian STS – Technology Development
Indian STS - Economics
Economic and Performance Analysis of Indian Space Transportation Systems
Economic and Performance Analysis of Indian Space Transportation Systems
Evolution of Indian Space Launch Vehicles Development
Economic and Performance Analysis of Indian Space Transportation Systems
PSLV – The Workhorse Indian STS
Economic and Performance Analysis of Indian Space Transportation Systems
GSLV – Medium Lifter to GTO
Economic and Performance Analysis of Indian Space Transportation Systems
SDSC-SHAR
First Launch Pad(PSLV)
Second Launch Pad(PSLV, GSLV, GSLV MK
III)
Third Launch Pad(HSF, RLV)
Solid Propellant Space Booster
Plant
Liquid Storage & Service
Facility
Vehicle Assembly and
Static Test
Quality & Reliability
Range Operations &
Control
Orbital Vehicle Preparation Facility Crew Training CenterManagement
Indian Space Launch Facilities - Satish Dhawan Space Center (SDSC)
Human Spaceflight ProgramObjectives: Develop a fully autonomous manned space vehicle to carry two crew to 400 km LEO and safe return to earth after mission duration of few orbits to 2 days extendable up to 7 days. Rendezvous and docking capability with space station/ orbital platform, safety provisions and provision for extra vehicular activity.
Timeline: 2016 (Launch by Indian GSLV)
Technology Development:Human Rated GSLV Rocket and Orbital Capsule
Crew Module and escape system (for 2 to 3)
Critical technology development areas, astronaut training, Vehicle Simulator
Collaboration with Russia for a 2013 Soyuz Mission with Indian cosmonaut and Technical cooperation
Indian Human Spaceflight Program (LEO Mission)
Economic and Performance Analysis of Indian Space Transportation Systems
STS - Technology DevelopmentATV:
Development of an air breathing propulsion (SCRAMJET) powered advanced technology vehicle (ATV) capable of placing 200-400 kg payloads up to an altitude of 800 km.
Research platform for studies of upper atmosphere and as a launch vehicle for Micro and Nano satellites.
RLV-TD:
Reusable Launch Vehicle – Technology Demonstration (RLV-TD) is conceived as a wing-body vehicle to be boosted by a rocket, that performs a hypersonic reentry for recovery from the Indian Ocean.
Economic and Performance Analysis of Indian Space Transportation Systems
Indian Space Program - Economics
Economic and Performance Analysis of Indian Space Transportation Systems
Indian Space Transportation Systems (STS) - Economics
Economic and Performance Analysis of Indian Space Transportation Systems
Comparison of Global Space Launch Vehicles
Economic and Performance Analysis of Indian Space Transportation Systems
Indian Space Program (ISP) Founding vision – Utilize space assets for socio-economic benefits Telecom (INSAT Series), Remote-Sensing (IRS Series), Meteorology Satellites Emerging Trend – Dedicated Space Exploration Missions and HSF Program Indigenous capability in Launch Vehicles and all facets of space exploration
Indian Space Transportation Systems (STS) PSLV Rockets for SSO (1,600 kg) and GTO (up to 1,000 kg payload) GSLV Rockets for GTO (2,500 kg) with Russian cryogenic upper stage GSLV mk2 with Indigenous cryogenic upper stage and GSLV mk3 (5,000 kg) Human Spaceflight Program (HSF) - First Mission by 2015-16 Development of semi-cryogenic engine, air breathing propulsion and
reusable launch vehicles in the next 5-6 years.
Findings & Conclusion
Economic and Performance Analysis of Indian Space Transportation Systems