Source Review: NASA OTPS — Space-Based Solar Power (Jan 2024)
Summary
| Verdict | Count |
|---|---|
| Consistent | 3 |
| Different conclusion | 1 |
| Merits investigation | 1 |
| Not relevant | 0 |
Claim 1: SBSP not competitive vs terrestrial under reference assumptions
Quote: Baseline LCOE $610-1,590/MWh vs terrestrial PV ~$84/MWh; optimistic-scenario $40-80/MWh.
Verdict: Consistent
Why: This is the authoritative skeptical position on SBSP commercial viability under current launch-cost regime. q6.c4 BAU 5 GW deployment is conditional on strategic-autonomy demand (non-LCOE) rather than commercial competitiveness, consistent with NASA's finding. The TAI-C 100 GW deployment requires the "optimistic scenario" of $40-80/MWh + sub-$200/kg launch + mass-production scaling — explicitly NASA's optimistic-corner case.
Claim 2: $100-200/kg launch threshold for SBSP viability
Verdict: Consistent
Why: This couples directly to q1's Starship cost-curve projection. Per q1's reviewed answer, $100-200/kg LEO is in the optimistic-late-2030s corner under partial-reuse, and is fully attainable only under TAI-grade compression. The launch-cost threshold IS the BAU-vs-TAI-C regime distinction for SBSP.
Claim 3: Capability-gap inventory (on-orbit assembly, autonomous
operation, beam-power hardware, GEO operations)
Verdict: Consistent
Why: These are the engineering bottlenecks that spaceambition-2026-sbsp also identifies (km-scale phased arrays as "hardest unsolved engineering risk"). Cross-corroborated.
Claim 4: Lifecycle emissions parity with terrestrial sustainable
Verdict: Different conclusion
Why: Where NASA OTPS finds emissions parity with terrestrial sustainables, scientificamerican-2026-sdc cites Saarland University researchers finding orbital DC could be "order of magnitude greater emissions" once launch and reentry are factored. The discrepancy is SBSP-vs-SDC scope (NASA is SBSP specifically; Saarland is broader orbital infrastructure including SDC). For q6 the emissions question is tangential to the mass-demand question, but flag for synthesis: emissions-driven regulatory regimes could cap orbital deployment volume regardless of launch cost.
Claim 5: Capability-gap closure path
Verdict: Merits investigation
Why: NASA OTPS identifies the gaps but does not endorse a closure path. Where does TAI-grade automation enter the closure? q3-isru already establishes a framework for acceleration-regime-dependent TRL progression; q6 should adopt the same framework for SBSP TRL. Cross-leaf consistency: q3's TAI-C / BAU / stall regimes map directly onto q6's SBSP deployment scenarios. Flag for synthesis.
Anti-hallucination check
- The LCOE ranges and $100-200/kg threshold are widely cited NASA OTPS figures, cross-validated via the spaceambition-2026-sbsp extract.
- Direct PDF not parseable via WebFetch; figures attributed via multiple secondary aggregators citing the report.
- Flag: future iteration should hand-extract the LCOE sensitivity tables for direct primary-source review.
Notes
NASA OTPS is the tier-S authoritative source on SBSP economic viability under reference assumptions. The skeptical finding is itself load-bearing for q6.c4's BAU-vs-TAI-C regime distinction. The optimistic-scenario LCOE $40-80/MWh creates the conditional under which 100 GW TAI-C deployment becomes commercially viable.