Hello friends,due to a discussion in the KitMaker Forum regarding my 'markings', where it was said that NASA used white duck tape, I was even more interested in these markings on the solar probe's cladding.
Even if the arrangement of these strips of different lengths may seem completely arbitrary and irregular at first glance, these markings must have had a purpose...
Quote from: roma847 on 04/28/2024 08:39 amHello friends,due to a discussion in the KitMaker Forum regarding my 'markings', where it was said that NASA used white duck tape, I was even more interested in these markings on the solar probe's cladding. ]It isn't "white duct" tape on the MLI/blankets but rather another type of tape.
Quote from: roma847 on 04/28/2024 08:39 amEven if the arrangement of these strips of different lengths may seem completely arbitrary and irregular at first glance, these markings must have had a purpose...They're pieces of fiberglass tape that reinforce the thermal blanket tie-downs. Apparently the Psyche spacecraft vendor liked to use that method, which I hadn't seen previously on spacecraft from other vendors.
I still think that they are some kind of tags of local positions of special equipment or sensors of the probe, especially since on some of them at high magnification one can see inscriptions that I have circled.
Be warned that the animation may not be very accurate in terms of the external blankets. For example, the imagers don't poke out nearly that much and are enclosed in a "doghouse" on the nadir panel. See https://www.flickr.com/photos/nasakennedy/53213102534/in/album-72177720298576586/ but there is a remove-before-flight cover over the apertures.
I mean this linkage next to the Hall-effect thruster.
BTW, I've read the linked article but found no references to your information regarding "... to correctly point the thrusters through the center of mass of the spacecraft, ..." But maybe I've missed the part.
Unlike Deep Space 1 and Dawn, which used the EP gimbals for direct attitude control of two axes while the EPthruster is operating, the Psyche GN&C uses RWAs for full 3-axis control even while thrusting. GN&C performsnominal RWA unloading and momentum control using torques generated by the EP system. The approach is similarto that used for Maxar's GEO communications satellites. The RWAs provide 3-axis control of the spacecraft attitudewhile a low-bandwidth momentum control algorithm positions the EP gimbal to direct the thrust vector near thevehicle center of mass. Small offsets to the EP thrust vector produce torques that allow near continuous unloading oftwo transverse axes of RWA momentum.