Why Reaching the Stars Is Physically Impossible — Brian Greene Explains
Where Physics Breaks
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Why Reaching the Stars Is Physically Impossible — Brian Greene Explains
2 547 просмотров · 4 дня назад
Where Physics Breaks
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2 547 просмотров · 4 дня назад
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Proxima Centauri is 4.243 light-years away — the nearest star to our Sun. At Parker Solar Probe speeds (163 km/s), the journey takes 7,800 years. But even with far better propulsion, physical constraints make the journey practically impossible for humans. Brian Greene develops every barrier with full quantitative rigor. The rocket equation: Δv = v_e × ln(m_i/m_f). For a 100-year journey to Proxima Centauri at ~0.085c average speed with fusion propulsion (v_e = 0.033c): mass ratio = e^{2.58} ≈ 13.2 (each way), total = (13.2)² ≈ 174 for a crewed round trip. For a 10,000 kg spacecraft: 1.74 million kg of fusion fuel. For antimatter propulsion (v_e = c): only 1,860 kg of antimatter needed — but global production is ~10⁻⁸ g/year; producing 1,860 kg at 10× global production would take 13 million times the age of the universe. Radiation at 0.085c: ISM protons arrive with 3.4 MeV kinetic energy, flux 2.55 × 10¹³ protons/m²/s, dose rate ~99 mSv/s (annual radiation worker limit in 0.5 seconds; lethal dose in 40 seconds). At 0.2c: electronics survivability — dose of 10⁷-10⁸ Gy over 20-year cruise vs. 100 Gy limit for radiation-hardened electronics. Dust impacts: at 0.5c, each 10⁻¹³ g grain delivers ~14 J to microscopic hull area; 1 impact per 2 hours on 100 m² cross-section. Biology of transit: bone mineral density loss at 1-2%/month in microgravity over 40 years; artificial gravity requires rotating habitat of ~100 m radius at ~3 rpm — massive engineering structure. Cosmic ray dose over 40-year transit at 0.1c: ~3 sieverts (exceeds NASA career limit). Specific proposals: Breakthrough Starshot (laser sailing to 0.2c) — 100 GW phased laser array unbuilt, electronics survivability unresolved; Project Daedalus (fusion ramjet to 0.12c) — requires 30,000 metric tons of He-3, vs. ~15 kg terrestrial reserves; Bussard ramjet — produces more drag than thrust (proton-proton chain is too slow for the required power density). Crewed interstellar missions require Type II civilization energy resources (~10¹³ × current human energy production).
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