Value chain · CLM-0668
In plain terms
The same company's own numbers show that, using the identical rocket and the identical (chemical) engine type throughout, simply choosing a higher orbit roughly quadruples the cost per kilogram - a separate effect from which propulsion type is used.
The claim as recorded
Virtus Solis's own model, holding launch vehicle (Starship) and propulsion type (chemical) constant, shows orbit choice alone driving a roughly 4x cost-per-kg multiplier: at 100 reuses, $9/kg to LEO, $26/kg to its own Molniya orbit (one tanker), and $35/kg to GEO (six tankers).
Scope and limits
T4, company's own unaudited model. Six tankers to GEO versus one to Molniya is itself a large driver of this ratio and is specific to Virtus Solis's own assumed satellite mass and orbital mechanics; this ratio should not be read as a general physical constant.
What it assumes
Both the Molniya and GEO cost figures use chemical tanker refuelling in the company's own model, so this isolates orbit choice from propulsion-architecture choice.
Where it comes from
, PDF p.14 (text layer): cost-per-kg-to-orbit table at varying Starship reuse counts, giving $9/kg (LEO), $26/kg (Molniya, one tanker), $35/kg (GEO, six tankers) at 100 reuses.
Basis: USD/kg, 2024 vintage, at stated Starship reuse counts
Related records
- Answers question
- QST-040 not published in this release
Cite this
energyaperture.com/c/clm-0668
CLM-0668, Energy Aperture, as of 2024.
Connected records
Other published records linked to this one. A list, not a judgement.
- Also from SRC-013
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