Mobility update

A brief update on PALADIN's mobility system:

The above is an early animation of the deployment of PALADIN's wheels. Details are available at our earlier post on Mobility.

We are currently looking at motors for PALADIN. There are a number of options we're looking at, with the following criteria (including gearhead):

Runs on less than 1W (up to 1.5 W acceptable)

Output step size at most half a degree - preferably smaller

Output rotational speed at least 2 rpm - preferably higher

Mass under 25 g per motor - preferably ~10 g

Diameter under 30 mm - preferably ~10 mm

Length under 50 mm - preferably ~30 mm

Minimizing step size allows careful positioning and keeps the rover in contact with the surface.
Maximizing rotational speed allows a higher maximum speed for longer traverses.


We are reaching out to space advocacy organizations and aerospace companies for support.

Phobos postcards! Thanks to Vistaprint.

Coming up next, a lengthy post on why we want to explore the Martian moons!

-Daniel

Focus On: Power Subsystem

A brief note on MarMoSet's power:

Mars will be near aphelion, its furthest point from the Sun, when MarMoSet arrives. Being 1.6 times further from the Sun than the Earth is, solar panels would provide only 36% of the power they would in Low Earth Orbit.

Our propulsion system, the ConstantQ hybrid electrostatic thruster, requires about 22 watts to operate. The thrusters would have to fire for extended periods due to their low thrust, so solar arrays must provide at least this much power. For this reason, we plan to use MMA Design's eHaWK array, which is the largest off-the-shelf CubeSat solar array.

Credit: MMA Design

With two wings, each with three 20 x 30 cm panels, the eHaWK provides 26 watts of power even at Mars. The arrays are gimbaled, so they can track the Sun as MarMoSet orbits, ensuring consistent power.

Such large arrays pose challenges for PALADIN, the mission architecture that includes roving on Phobos's surface. Even if the arrays are strong enough not to be broken or mangled during landing, they could easily get caught on the terrain, prematurely ending PALADIN's mission. For this reason, the two large wings will detach from the spacecraft during its final approach of Phobos (confirmed feasible by MMA). Once landed, the nanorover no longer requires enough power to operate its thrusters, which in any case would not be capable of lifting it off Phobos's surface.

PALADIN (and possibly the orbiter-only architecture, DELPHI) would therefore also have a body-mounted solar panel on its upper 6U face. Depending on the model, this array would provide at least 4.3 - 7.2 watts at solar noon.

MarMoSet will also carry batteries to provide the spacecraft with power during nights on Phobos. We are still deciding how much storage is necessary, but are currently planning to store 40 Wh, enough to fire the thrusters at full power for nearly two hours and to provide PALADIN with power for a full Phobos day.

Credit: Clyde Space

Depending on orbital planning and volume available, we may increase energy storage capacity. Two 10 Wh batteries would likely fit on either side of the NAC's optical tube..

That's all for now! We're currently working on flight computers, Mars capture, and nanorover motors, posts on each likely coming soon!

-Daniel