Shall
NASA be Able to Re-position an Asteroid?
Summary: NASA has recently announced its
intention to capture an asteroid and re-position it close to moon, to be used
as space station. However several conditions need to be taken into
consideration to accomplish the task and hence it may really not be possible
for NASA to meet its stated objectives.
American space agency has recently announced
its intention to re-position an asteroid close to moon in an orbit and use it
as a space station. NASA has claimed that it has all the technology to
accomplish the task. It is expected to serve as a proving ground for hardware
and crews en route to larger objects deeper into space.
In April, the Keck Institute for Space Studies
at the California Institute of Technology reported its conclusion that a 5,
00,000-kg (1.1-million-lb.) near-Earth asteroid (NEA) could be discovered,
tracked, captured and delivered to cislunar space by 2025 at a cost of about
$2.65 billion.
Keck concluded that placing a 500-ton asteroid
in high lunar orbit could provide a unique, meaningful and affordable
destination for astronaut crews in the next decade. This disruptive capability
would have a positive impact on a wide range of space exploration interests,
which includes developing technology to deflect an asteroid on its way to a
disastrous collision with Earth’s atmosphere.
Astronomers on the Keck team estimated that a
“low-cost, ground based observation campaign” could identify five or so
candidate targets per year in the desired 7-meter-dia. Range.
A spacecraft generating power with large circular
“Mickey Mouse” solar arrays would use Xenon-based 10-kw Hall thrusters to
spiral out to the desired NEA – firing four at a time, each with a specific
impulse of 3,000 sec. As it approaches the target, it would use on board
instruments to characterize its shape and rotation, and apply algorithms
developed by the Defense Advanced Research Agency to match its spin. Then it
would essentially lasso the NEA with a 15-meter dia. “capture bag” that would
be clinched tight over the spinning space rock, once the spacecraft and
asteroid are tightly secured together, the spacecraft would then de-tumble the
combination. The Keck study experts calculate that it would take 300 kg of
propellant to stabilize the asteroid.
After that, the spacecraft could use its solar-electric
propulsion to work its way into a high lunar orbit or even one of the Earth-
Moon Lagrangian points that NASA is studying as way stations that avoid
fuel-consuming gravity wells en route to destinations beyond low Earth orbit.
It is well known that all celestial bodies
maintain precise elliptical orbits. A circular orbit can easily be understood
on the basis of balance of gravitational force of attraction and centrifugal
force but elliptical orbits that are precisely maintained over an immense period
of time can’t be thus explained. No doubt, Kepler’s laws of planetary motion
have sufficient room for elliptical orbits but they only define the conditions
that are met and not the mechanisms utilized to meet the conditions. It is
implicit even in ‘Kepler’s equal area law’ that elliptical orbit requires
mathematically-precise maintenance. There is really no room for a celestial
body to wander about its elliptical path. Elliptical orbits, for example,
involve precise movement of Earth towards Sun during part of its journey and
precise movement of Earth away from Sun during another part of its journey. Not
only this, it also involves precise conservation of total energy of a celestial
body all the time. Therefore elliptical movement of celestial bodies is quite
unlike the pendulum movement which involves total inter-conversion of kinetic
energy into potential energy and vice versa. Elliptical orbits of celestial
bodies involve mathematically precise partial inter-conversion of kinetic
energy and potential energy. We just don’t know as to how celestial bodies
conserve their energy, maintain precise elliptical paths, precisely regulate
inter-conversion of kinetic energy into potential energy and vice versa; and
precisely move towards or away from their Sun.
Re-0positioning an asteroid into a new orbit
demands precise understanding of these considerations so that appropriate
technology can be developed to meet above stated considerations. However, since
astronomers/physicists have never posed these questions to themselves,
therefore there can’t be any solutions to these questions either.
Hence, NASA may have the technology to be able
to discover, track, capture and deliver an asteroid to cislunar space but it is
unlikely to have technology to keep it in cislunar space along a precise
mathematically predictable elliptical orbit. This must be true and correct at
the present level of understanding and technology development.
Therefore NASA with all its resources is
unlikely to be able to re-position an asteroid into a new home. Yet this
technology may be useful to deflect an asteroid on its way to a disastrous
collision with Earth’s atmosphere.
Author: Dr Mahesh C. Jain is a practicing
medical doctor has written the book “Encounter of Science with Philosophy – A
synthetic view”. The book begins with first chapter devoted to scientifically
valid concept of God and then explains cosmic phenomena right from origin of
nature and universe up to origin of life and evolution of man. The book
includes several chapters devoted to auxiliary concepts and social sciences as
corollaries to the concept of God. This is the only book that deals with origin
of nature and universe from null (Zero or nothing). This article is in line
with author’s understanding of nature.