Aryavarta - A novel approach towards innovative and efficient space transportation systems

Paper number

IAC-10.D3.2.6

Author

Dr. Rushi Ghadawala, Aryavarta Space Organization, India

Coauthor

Mr. Poojan Chokshi, Aryavarta Space Organization, India

Coauthor

Mr. Chiragkumar Tala, Aryavarta Space Organization, United States

Coauthor

Mr. Kedar Pithwa, Aryavarta Space Organization, United Kingdom

Year

2010

Abstract

With the advancement of technology, there is a growing interest about other planets and so it would
be necessary to shift the scientific analysis activities from the earth’s orbit to that of other planets. The
main aim of project ARYAVARTA is to shift a satellite orbit from one planet to another with the help
of an Unmanned Space Vehicle (USV). For example, to shift scientific activities economically to other
planets, we need to change the orbit of the satellite from earth to that of the other planet instead of
sending separate space probes, as that would entail comparatively much higher cost.
A solar powered USV is one that will be having ion propulsion system along with solar propulsion
system. The USV, placed in rocket boosters, will be externally launched like a space shuttle to enable it
to go beyond the atmospheric limit of the earth with sufficient escape velocity. Xenon cylinders attached
to the USV will provide ion propulsion for furthering the mission. The USV will then be attached to
the satellite revolving in the orbit of the earth. The satellite which is attached to the USV will be deorbited
with the help of xenon engines, and will be shifted to another orbit of another planet/satellite.
Electricity generated by solar panels, made from multicrystalline solar cells, of the USV will be stored
in the USV to help the mission/operational requirements. With the help of multireflectors, the reflected
solar rays will be re-concentrated to the solar panel and hence, power efficiency will increase more than
twice. Solar-electromagnetic propulsion would make such a mission possible because an ion engine can
run almost continuously and outperform any chemical rocket for such long flights. This project will help
to achieve higher efficiency with great economy, and eliminate the need for sending extra space probes
for any other mission. As xenon engine occupies lesser room than conventional engines, more compact
instruments will emerge ahead resulting in the overall reduction of the size and mass of the spacecraft,
and thereby further increasing efficiency of the spacecraft.

Abstract document

IAC-10.D3.2.6.brief.pdf

Manuscript document

IAC-10.D3.2.6.pdf (🔒 authorized access only).

To get the manuscript, please contact IAF Secretariat.