Spacecraft Honeycomb
Spacecraft Honeycomb
(OP)
Hi, would like to know if non-metallic composite honeycomb is suitable for satellite?
I have seen most of the example projects, limited to my access, are using Al composite honeycomb...
Thank you!
I have seen most of the example projects, limited to my access, are using Al composite honeycomb...
Thank you!
RE: Spacecraft Honeycomb
another day in paradise, or is paradise one day closer ?
RE: Spacecraft Honeycomb
I don't see any much project example using CFRP with aluminum honeycomb except the following...
https://earth.esa.int/web/eoportal/satellite-missi...
https://www.nasa.gov/mission_pages/maven/news/mave...
RE: Spacecraft Honeycomb
another day in paradise, or is paradise one day closer ?
RE: Spacecraft Honeycomb
TTFN (ta ta for now)
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RE: Spacecraft Honeycomb
Honeycomb panels are used extensively for launch vehicle jettisonable fairings and inter-stage parts... but most satellite structure relies on monolithic sheets/panels. BTW the honeycomb panels in these cases are made for noise/vibration control/deadening and are 'naturally vented' to quickly vent-off internal core-cell air pressure during high friction/heating ascent and reducing atmospheric pressure to '0'... using perforated honeycomb core materials... that could be composite/paper and aluminum foils/cell-walls, as design dictates. This could extend to other expendable components that would have limited critical structural performance life and will be jettisoned later in the flight profile.
I think the reasons for using monolith parts [primarily metallic] for the dedicated spacecraft... that are integral [integrally made] and then sections fastened together... is to eliminate any reliance on adhesive bonding in the harsh environment of space, which is known to degrade most non-metallic materials... heat-cold, radiation, atomic gasses/ions, etc... and makes long-term absolute structural integrity for critical composite and bonded assets impossible to be validated as 100% reliable. The ONLY exception to this might be stainless steel or titanium perforated honeycomb core and face-sheet/skin panels that are welded or brazed together... not adhesive-bonded.
NOTES1:
a. Spacecraft are subject to venting of trapped gasses for days/weeks/years from every micro-voids/pore... and honeycomb and composite materials [especially composite/paper honeycomb] are especially vulnerable to this phenomena.
b. The plastic body Tesla that SpaceX launched into inter solar space is predicted to soon-be a mass of fragile junk, as it comes-apart, because of non-metallic materials degradation.
c. The [4] landing gear struts for the Apollo lunar modules used a honeycomb filler material for struct shock attenuation [by crushing/compacting] on lunar landing... but they were never intended for long-duration exposure, before fulfilling their 1-time critical function.
d. If trapped air is subject to deep-cryogenic temperatures, the it will usually liquify... forming LN2, LO2, LAr2, etc. Now, imagine what happens if liquified gases are suddenly exposed to high aero-friction heating... when trapped in core cells or even small voids???!!!!
e. I am pretty sure that even interior panels of the ISS are NOT honeycomb for a multitude of reasons, that are far-beyond this discussion.
f. Hint (e)… one-of many other serious issues. SAE AIR5661 Compartment Decompression Analysis is worth reading... everything blows apart in incredible and scary ways... and structural integrity is really hard to maintain.
NOTE2.
In the 1990s a unique materials experiment was placed into orbit by a Space Shuttle... the [huge] Long Duration Exposure Facility. The LDEF exposed hundreds of materials [including coatings, insulation, plastics, wires, etc] to low earth orbit. LDEF was designed to 'stay-up' just for ~1 year... but due the loss of the SS Challenger... spent many years in LEO before it was retrieved by another Space Shuttle. It was a gold-mine for materials performance in the harsh space LEO environment. The subsequent reports of findings are in several very interesting NASA/CR reports... although some findings may [still] be classified.
Gotta-go-back-to-work...
Regards, Wil Taylor
o Trust - But Verify!
o We believe to be true what we prefer to be true. [Unknown]
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RE: Spacecraft Honeycomb
Does perforated honeycomb core give different properties compared to same spec but non-perforated honeycomb core?
The Hexcel spec highlight the the honeycomb cell wall has perforated and non-perforated but the mechanical properties are for general honeycomb core... does it mean perforated cell wall no impact on the properties?
https://www.hexcel.com/user_area/content_media/raw...
RE: Spacecraft Honeycomb
it could also be that it (perforation) helps potting compound to penetrate the core better.
"Hoffen wir mal, dass alles gut geht !"
General Paulus, Nov 1942, outside Stalingrad after the launch of Operation Uranus.
RE: Spacecraft Honeycomb
TTFN (ta ta for now)
I can do absolutely anything. I'm an expert! https://www.youtube.com/watch?v=BKorP55Aqvg
FAQ731-376: Eng-Tips.com Forum Policies forum1529: Translation Assistance for Engineers Entire Forum list http://www.eng-tips.com/forumlist.cfm
RE: Spacecraft Honeycomb
Most hex core is made by bonding sheets, then expanding the bonded sheet stack into hex shapes.
RE: Spacecraft Honeycomb
Cheers
Greg Locock
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RE: Spacecraft Honeycomb