Energy Aperture

Value chain · CLM-0882

In plain terms

For low Earth orbit NASA gives a voltage above which a power system may arc. For geostationary orbit it gives no equivalent voltage at all - the limits are set on how many electrons accumulate in a material and how strong the electric field inside it gets. The two orbits are not constrained in the same terms.

The claim as recorded

NASA's design guidance for geostationary orbit states its charging constraints in electron fluence and dielectric field strength rather than in bus voltage: protect dielectrics and circuits to the level of 10^10 electrons per square centimetre per 10 hours, keep dielectric fields below 100 volts per mil, treat 110 mils of grounded aluminium as usually sufficient shielding for GEO orbits, and treat dielectrics as adequately leaky at 10^9 ohm-centimetres if grounded. This guidance states no GEO bus-voltage threshold.

Evidence behind this: NASA handbook summary paper read directly in the held file. The four figures were read from a rendered page, not from the text layer, which corrupts each of them.

Scope and limits

THIS IS INTERNAL, DEEP-DIELECTRIC CHARGING GUIDANCE AND IT IS NOT A SAFE-VOLTAGE LIMIT. It does not state that any bus voltage is safe or unsafe in GEO, and it may NOT be used to clear or condemn the 40 kV of CLM-0210 or the 5 kV of CLM-0879. 100 V/mil is about 3.9 MV/m and constrains the field across an insulator, which is a function of voltage AND insulation thickness, so no bus voltage follows from it without a stated thickness this source does not give. The guidance is dated 2000 and addresses spacecraft two to three orders of magnitude smaller than any SPS design in the register. THE FIGURES ARE IMAGE-READ BECAUSE THE TEXT LAYER CORRUPTS THEM, rendering 100 V/mil as "100 V/rail".

What it assumes

No assumptions are recorded against this claim.

Where it comes from

SRC-443 NASA's Technical Handbook for Avoiding On-Orbit ESD Anomalies Due to Internal Charging Effects,...
Read on the rendered page 3 of the held file: "110 mils of aluminum (grounded) is usually sufficient for GEO orbits"; "protect dielectrics and circuits to the level of 10^10 e/cm2 per 10 hours"; "keep dielectric fields below 100 V/mil"; and "use dielectrics that are leaky (10^9 ohm-cm, and grounded, is good enough)".

Basis: GEO internal charging environment

Related records
Answers question
QST-043 not published in this release

Cite this

energyaperture.com/c/clm-0882

CLM-0882, Energy Aperture, as of 2000.

Connected records

Other published records linked to this one. A list, not a judgement.

Also from SRC-443
CLM-0883NASA puts the level at which internal charging starts causing failures at twenty billion electrons per square centimetre over ten hours...