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Propulsion software for spacecraft — engines, tanks, burn plans, executed burns with Tsiolkovsky Δv, abort feasibility, and a live Δv budget tracker.

Propulsion software for spacecraft — engines, tanks, burn plans, executed burns with Tsiolkovsky Δv, abort feasibility, and a live Δv budget tracker.

What's included

Engine + tank registry per vehicle — bipropellant / monopropellant / solid / electric / cold-gas / nuclear-thermal

Burn plans with target Δv, planned TIG, duration, throttle setpoint

Executed-burn logging — Δv computed via Tsiolkovsky from propellant + initial vehicle mass + engine Isp

Server-side burn trigger transactionally decrements fuel + oxidizer tanks by mixture ratio, updates vehicle currentPropellantPct, bumps engine cycles

Performance alarms — under/over-performance vs. target Δv at warning + critical thresholds; critical → Mission anomaly mirror

Abort modes with required Δv + propellant; feasibility recomputes live as tank state changes (feasible / marginal / infeasible)

Δv budget tracker — budget vs. expended vs. reserved-for-armed-aborts vs. available with stacked-bar visualization and live verdict

Daily health scan: engines approaching qualified-cycle limit, tanks below reserve

Wally tools: list engines, Δv budget, upcoming burns, abort feasibility, plan-burn, log-executed-burn

About this module

Propulsion is what propulsion engineers reach for instead of a spreadsheet. Engine + tank registry per vehicle (bipropellant, monoprop, solid, electric, cold-gas, nuclear-thermal). Burn plans with target Δv + TIG + duration + throttle setpoint.

Executed-burn logging — actual Δv computed via Tsiolkovsky from propellant + initial vehicle mass + engine Isp. Abort feasibility recomputes live as state changes. Live Δv budget tracker (budget vs. expended vs. reserved-for-aborts vs. available).

What you can do with it

  • Plan a Mars-injection burn with throttle profile + abort-feasibility check

  • Log an actual on-orbit burn and update the remaining Δv budget

  • Watch the Δv reserve dwindle through a multi-burn rendezvous sequence

  • Compare electric vs. chemical propulsion options for a deep-space mission

Get this module

Free for all Turtini organizations.

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Who it's for

  • Space-mission propulsion engineers
  • Smallsat + cubesat teams
  • Aerospace students + faculty running mission-design coursework

Details

Category
Operations
Pricing
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