MXER Tether-Assisted Reusable Launcher
Orbital Launch System Pitch
A reusable suborbital LH2/LOX booster paired with an in-orbit momentum-exchange tether that circularizes the payload into LEO and reboosts on solar power. Every number is computed from real lab engines already in this app — equation-backed, nothing invented.
13 sections · equations · vector diagrams · mass & cost budgets · lab-sourced data tables
Orbital velocity (200 km)
7,784m/s
Δv rocket (suborbital)
8,675m/s
Δv tether supplies
784m/s
Propellant fraction
86.0%
Tether tip / period
801s
Reboost time
24.2hr
Risk P95 loss
$37.6M
Carbon / launch
283kg CO2e
v = sqrt(μ / r) μ = 3.986e14, r = R⊕ + h Δv = Isp · g0 · ln(m0 / mf) (Tsiolkovsky) mp/m0 = 1 − e^(−Δv / (Isp·g0)) (propellant fraction) v² = μ (2/r − 1/a) (vis-viva) v_tip = ω · L (rotovator tip speed) taper = e^(v_tip² / 2·(σ/ρ)) (tether material) ΔE = ½·m·(v_orb² − v_sub²) (reboost energy)
No-Fibs — What This Lab Really Does
This is a conceptual engineering pitch, not a flight-qualified design. The orbital-mechanics equations (Tsiolkovsky, vis-viva, Hohmann, Oberth) are real textbook physics. Every data point — material suitability, risk RPNs, supply-chain resilience, carbon factors, energy-grid metrics — is computed live by the real lab engines in The Human Brain App, each grounded in published standards (MatWeb, EPA eGRID, IEC 60812, ISO 31000, ISO 28000, GHG Protocol). The MXER tether concept draws on published momentum-exchange work (Forward, Hoyt); Zylon data is Toyobo's spec. Nothing here has flown. The PDF is an honest projection from real physics, labeled as such — no fabricated heritage, no invented performance numbers.