Energy Aperture

Value chain · CLM-0257

In plain terms

For every kilogram of hardware launched into orbit over the station's 30-year life, RD1 generates about 30,000 kilowatt-hours of electricity, and RD2 about 17,500.

The claim as recorded

Over a 30-year system life, RD1 delivers approximately 30,122 kWh of electricity per kg of hardware launched (including refurbishment mass), and RD2 delivers approximately 17,537 kWh/kg.

T0 own calculation · medium confidence · as of 2026-09 · VER-157 CONFIRMED 2026-09-03 · XC02

Scope and limits

A physical consistency check only; does not establish whether this is a favourable or unfavourable ratio without a comparator, and the terrestrial-PV comparator figure quoted in the trace (order 10^4-10^5 kWh/kg) is ASSUMED/illustrative, not a cited study result.

What it assumes

Total hardware mass launched over the lifecycle includes the initial build plus both refurbishment cycles (3x initial upmass for RD1, 3x for RD2), consistent with the launch-count derivation in CLM-0243.

Where it comes from

SRC-012 Space Based Solar Power., 2024

This is the project's own working, shown in full:

CALC-058 Physical sanity check: delivered energy per kilogram launched
Trace, Section 9: RD1 5.332e11 kWh / 17,700,000 kg = 30,122 kWh/kg; RD2 5.314e11 kWh / 30,300,000 kg = 17,537 kWh/kg.

Basis: physical units (kWh/kg), no currency; 30-yr system life

Related records
Answers question
QST-038 not published in this release

Cite this

energyaperture.com/c/clm-0257

CLM-0257, Energy Aperture, as of 2026-09.

Connected records

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

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More on the source page.