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OVERVIEW
The project aims to demonstrate a concept for advanced nano-spacecrafts attaching to lightsails and using the possibility of light-powered space travel at high speeds (significant fraction of light speed), and advanced nanotechnology. Along with theirs nanolanders (nanorobots) that can withstand extreme environment of planets and moons, these nano-spacecrafts will perfom these detailed studies :
Moreover, this project guarantee a low-cost execution of critical missions, and that will be gainful in all sides.
TECHNOLOGY
The Multi-Mission Nanospacecraft prototype
To validate the architecture, The pathfinder mission is using a standard 3U CubeSat with a size of 10 cm x 10 cm x 30 cm and a mass of < 5 kg. Currently, we are working on an extensive use of MWCNT-based composite structures.
ADCS (Attitude Determination and Control Subsystem)
The ADCS consists of a set of sensors, actuators and a microcontroller with the algorithms, utilizing a combination of a single pitch wheel and four torque coils. The attitude knowledge is derived through a combination of sun sensors and a magnetometer. The ADCS demonstrate the following capabilities :
Power and Thermal management
A set of four double-sided, MWCNT flexible solar arrays are oriented such that there is no spacecraft orientation in which energy generation is not possible. Across all sun-orbit beta angles, the system is capable of generating greater than 6 W of orbit average power. To maximize electric power transfer between the solar cell strings and the lower-voltage spacecraft power bus (battery), a peak-power-tracking power converter, developed particularly for nanospacecrafts, is used. Several DC–DC converters produce regulated bus voltages for use by the spacecraft and payload. A high-capacity lithium ion battery supports mission operations that require as much as 50 W peak power for durations up to 10 min per orbit, including during eclipse.
Command and Data Handling
To provide scalable processing capability for the Nanospacecraft command and data handling subsystem, a radiation-hard Aeroflex 32 bit LEON 3-FT processor is used. The LEON processor-based avionics, with its associated circuitry, is capable of extended operation under extremely stressing radiation, both total ionizing dose and single-event upsets and latchups, and environmental conditions
Communication
Nanospacecrafts X-band communications system is the spacecraft’s link to Deep Space Network (DSN), returning science data, exchanging commands and status information, and allowing for precise radiometric tracking through NASA’s Deep Space Network of antenna stations.
Nanosensors
Machine Learning
Nanospacecrafts use Machine Learning to :
- Compare data of microorganism existing on earth to extraterrestial microorganism (ex : in europa moon)
- Remove known false positives
- Align astrometry of newly observed objects
fB = 0.03 x E-4/5 , fB : annual frequency of impact, E : energy of impact
R = Pi / fB x DT , R : relative risk, Pi : probability of impact, DT : time (year)
PS = log10 x R , PS : Palerme Scale
PS < -2→ no risk
-2 <PS < 0 → possible risk
PS > 0 → a threat
NEOs Deflection
The NEOs deflection method consists in focusing sunlight onto an asteroid with space-based mirrors wich heat the asteroid’s surface to more than 2100° C to start vaporising it.
Cleaning space
The Japanese Aerospace Exploration Agency proposes to use an electrodynamic tether whose current would slow down the speed of satellites or space debris, slowing the satellite speed would make it gradually fall closer to Earth, where it will burn up.
Laser-Ablation Propulsion : A More Practical Concept
LASER ablation propulsion (LAP) is a major new electric propulsion concept. . In LAP, an intense laser beam [pulsed or continuous wave (CW)] strikes a condensed matter surface and produces a jet of vapor or plasma. Nanopacecrafts can be propelled in this way. So this propulsion system pushed sails, allow the possibility of fuel-free propulsion in space. This makes possible missions to a nearby star.
Material : Mylar
Thickness : 4.5 microns
Layout : Four triangular sails forming a square, connected with four tape-measure-like booms.
Boom length : 4 m
LightSail width : 5.6 m
Total sail area : 32 m²
The entire lightsail structure would be accelerated at 30% of Earth gravity by 43,000 terrawatts of laser power. At this acceleration, the lightsail would reach a velocity of half the speed of light (150000 km/ s) in 1.6 years.