Analysis
The question DAG decomposed into Input Questions (atomic factual leaves), Analyses (synthesis nodes that combine inputs), and Side Chapters (constraint or orthogonal deep-dives).
Question DAG click any node to jump to its leaf
graph TD classDef root fill:#fafaf7,stroke:#c4622d,stroke-width:2.5px,color:#1a1a1a,font-weight:bold; classDef leaf fill:#fafaf7,stroke:#4a4a4a,stroke-width:1px,color:#1a1a1a,font-weight:bold; classDef leafDone fill:#e8f3ee,stroke:#2d6a4f,stroke-width:1.5px,color:#1a1a1a,font-weight:bold; classDef leafInProg fill:#fef3e3,stroke:#d97706,stroke-width:1.5px,color:#1a1a1a,font-weight:bold; classDef synthesis fill:#f0efe9,stroke:#4a4a4a,stroke-width:1px,color:#1a1a1a,font-weight:bold; classDef constraint fill:#fafaf7,stroke:#9ca3af,stroke-width:1px,stroke-dasharray:4 3,color:#1a1a1a,font-weight:bold; root["Root question"] click root "/lunar-throughput-multiplier/" "Does building a base on the Moon increase the total mass throughput humanity can deliver to elsewhere in the solar system — and at cosmic scales (Tt/yr), what constraints bind first on each side?" class root root; q1_earth_industrial_ceiling["Earth industrial ceiling (6/6)"] root --> q1_earth_industrial_ceiling click q1_earth_industrial_ceiling "/lunar-throughput-multiplier/leaves/q1-earth-industrial-ceiling/" "What is the Earth-launch throughput ceiling imposed by industrial inputs (LOX, methane, engine production, pad cadence, stainless steel, ASU power) for chemical rockets — at what kt/yr or Mt/yr to LEO" class q1_earth_industrial_ceiling leafDone; q2_earth_atmospheric_ceiling["Earth atmospheric ceiling (3/6)"] root --> q2_earth_atmospheric_ceiling click q2_earth_atmospheric_ceiling "/lunar-throughput-multiplier/leaves/q2-earth-atmospheric-ceiling/" "What is the Earth-launch throughput ceiling imposed by atmospheric chemistry — ozone depletion (Cl, BC, NOx), stratospheric water-vapor injection, reentry metal injection (alumina, Na, Fe), and therma" class q2_earth_atmospheric_ceiling leafInProg; q3_earth_destination_reachability["Earth destination reachability …"] root --> q3_earth_destination_reachability click q3_earth_destination_reachability "/lunar-throughput-multiplier/leaves/q3-earth-destination-reachability/" "For each propulsion class — (a) chemical methalox (Starship-like primary regime), (b) electric / ion propulsion stages, (c) nuclear thermal rockets (NTR), (d) nuclear pulse propulsion (NPP / Orion-sty" class q3_earth_destination_reachability constraint; q4_lunar_power_ceiling["Lunar power ceiling (0/6)"] root --> q4_lunar_power_ceiling click q4_lunar_power_ceiling "/lunar-throughput-multiplier/leaves/q4-lunar-power-ceiling/" "(DEPRECATED) What is the achievable power-supply ceiling for a mature lunar industrial base?" class q4_lunar_power_ceiling leaf; q5_lunar_materials_ceiling["Lunar materials ceiling (0/6)"] root --> q5_lunar_materials_ceiling click q5_lunar_materials_ceiling "/lunar-throughput-multiplier/leaves/q5-lunar-materials-ceiling/" "What is the lunar regolith mining + processing rate ceiling at industrial maturity, and what fraction of launched mass must remain Earth-shipped 'vitamin' material (copper, REE, polymers, electronics," class q5_lunar_materials_ceiling leaf; q6_mass_driver_throughput["Mass driver throughput (0/6)"] root --> q6_mass_driver_throughput click q6_mass_driver_throughput "/lunar-throughput-multiplier/leaves/q6-mass-driver-throughput/" "What is the throughput ceiling of a mature lunar mass-driver architecture — first-principles power → kg/s for a single driver (accounting for duty cycle, cycle-life, thermal dissipation in vacuum, pay" class q6_mass_driver_throughput leaf; q7_receiver_infrastructure["Receiver infrastructure (0/6)"] root --> q7_receiver_infrastructure click q7_receiver_infrastructure "/lunar-throughput-multiplier/leaves/q7-receiver-infrastructure/" "(DEPRECATED) What catcher/receiver infrastructure is required?" class q7_receiver_infrastructure constraint; q8a_moon_propellant_for_earth_launched["Q8a moon propellant for earth l…"] root --> q8a_moon_propellant_for_earth_launched click q8a_moon_propellant_for_earth_launched "/lunar-throughput-multiplier/leaves/q8a-moon-propellant-for-earth-launched/" "If the Moon uses its entire propellant-production capacity to supply LOX/LH2/H2O/etc. to LEO and cislunar (rather than burning it on Moon-launched cargo): how much does Earth-launched cargo's effectiv" class q8a_moon_propellant_for_earth_launched leaf; q8b_moon_propellant_for_moon_launched["Q8b moon propellant for moon la…"] root --> q8b_moon_propellant_for_moon_launched click q8b_moon_propellant_for_moon_launched "/lunar-throughput-multiplier/leaves/q8b-moon-propellant-for-moon-launched/" "If the Moon uses its entire propellant-production capacity on Moon-launched cargo (mass-driver-boosted-then-burned chemical/NTR upper stages, or fully propulsive chemical/NTR ascent from regolith): ho" class q8b_moon_propellant_for_moon_launched leaf; q9_synthesis_cosmic_multiplier["Synthesis cosmic multiplier (0/…"] root --> q9_synthesis_cosmic_multiplier click q9_synthesis_cosmic_multiplier "/lunar-throughput-multiplier/leaves/q9-synthesis-cosmic-multiplier/" "Integrating Earth ceilings (q1, q2), propulsion-class destination reachability (q3), lunar materials (q5), mass-driver throughput including parallelization and brief receiver discussion (q6), and the " class q9_synthesis_cosmic_multiplier synthesis;
Input Questions (Leaf)
- q1-earth-industrial-ceiling What is the Earth-launch throughput ceiling imposed by industrial inputs (LOX, methane, engine production, pad cadence, stainless steel, ASU power) for chemical rockets — at what kt/yr or Mt/yr to LEO does each input bind?answered
LOX binds first — soft ceiling ~120 launches/yr (5% US O2), hard ceiling ~2,330/yr. Engines second (~2,600/yr at current target × 100-flight reuse), pads third (~18-55k/yr). With civilizational-scale mobilisation the Earth chemical ceiling sits at 1-100 Mt/yr LEO; Tt/yr cosmic scale is 1-3 OOM beyond and unreachable from Earth chemical alone.
16 sources · 20 claimsjust now - q2-earth-atmospheric-ceiling What is the Earth-launch throughput ceiling imposed by atmospheric chemistry — ozone depletion (Cl, BC, NOx), stratospheric water-vapor injection, reentry metal injection (alumina, Na, Fe), and thermal forcing — distinguishing launch from reentry, at what launches/yr or kt/yr does each effect become climate or ozone binding?answered
Atmospheric chemistry binds Earth chemical-rocket throughput at ~100 Mt-1 Gt/yr LEO (10^6-10^7 launches/yr); anchored on Larson 2017's chemistry-climate modeling of high-cadence hydrogen-propellant launches. 10-100× lower than q1's solar-PV ceiling, making atmospheric chemistry the load-bearing Earth-side constraint. Methalox is cleaner than current mixed fuel mix but not architecture-redesignable — reentry NOx + stratospheric H2O perturbation are fundamentally physical. The Handmer solar-abundance regime does not relax q2 because synthetic methane combustion is chemically identical to fossil methane combustion.
6 sources · 8 claimsjust now - q4-lunar-power-ceiling (DEPRECATED) What is the achievable power-supply ceiling for a mature lunar industrial base?0/6 done0 sources
- q5-lunar-materials-ceiling What is the lunar regolith mining + processing rate ceiling at industrial maturity, and what fraction of launched mass must remain Earth-shipped 'vitamin' material (copper, REE, polymers, electronics, lubricants) — does that fraction shrink with closure or asymptote at a non-trivial floor?0/6 done0 sources
- q6-mass-driver-throughput What is the throughput ceiling of a mature lunar mass-driver architecture — first-principles power → kg/s for a single driver (accounting for duty cycle, cycle-life, thermal dissipation in vacuum, payload g-load tolerance), and what happens when the cycle-life or thermal limit on a single driver is reached and the response is to build N parallel drivers? Anchor against Casey Handmer (May 2026) and the NASA SP-428 / O'Neill lineage. Briefly assess whether catcher/receiver infrastructure at the destination is a paired binding constraint, or whether self-propelled payloads route around it.0/6 done0 sources
- q8a-moon-propellant-for-earth-launched If the Moon uses its entire propellant-production capacity to supply LOX/LH2/H2O/etc. to LEO and cislunar (rather than burning it on Moon-launched cargo): how much does Earth-launched cargo's effective rocket-equation tax to Mars/NEAs/Belt/outer destinations fall, and what is the resulting throughput multiplier per Earth launch — relative to Earth-direct?0/6 done0 sources
- q8b-moon-propellant-for-moon-launched If the Moon uses its entire propellant-production capacity on Moon-launched cargo (mass-driver-boosted-then-burned chemical/NTR upper stages, or fully propulsive chemical/NTR ascent from regolith): how much interplanetary throughput does Moon-as-launcher deliver, and how does that compare to the Moon-as-supplier case (q8a)?0/6 done0 sources
Analyses
Side Chapters
Structural or orthogonal deep-dives surfaced during research. Could materially shift the bottom line but live outside the main DAG.
- q3-earth-destination-reachability For each propulsion class — (a) chemical methalox (Starship-like primary regime), (b) electric / ion propulsion stages, (c) nuclear thermal rockets (NTR), (d) nuclear pulse propulsion (NPP / Orion-style) — and for both Earth-launched and Moon-launched cargo: what fraction of LEO (or Moon-surface) mass reaches each destination (GEO, cislunar, Mars, NEAs, Belt, Jovian, Mercury, sundivers), and which destinations are categorically unreachable from each side under each propulsion class?0/6 done
- q7-receiver-infrastructure (DEPRECATED) What catcher/receiver infrastructure is required?0/6 done