Vessel Viewer KSP

A precise tool for KSP players and designers to analyze vessels by calculating delta-v, mass, and thrust-to-weight, with a visual vessel viewer.

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About This Tool

Purpose & User Intent: The Vessel Viewer KSP tool addresses the need to quickly quantify and visualize Kerbal Space Program vessel configurations. Target users are KSP players, educators, and designers who want immediate feedback on flight viability and design trade-offs without running a full simulator. Use when comparing vessels, planning missions, or teaching propulsion concepts.
Core Logic & Features: The tool ingests vessel parameters such as dry_mass_kg, propellant_mass_kg, payload_mass_kg, Isp_s, engine_thrust_kN, total_mass_kg, and environment flags (gravity_scale, atmosphere). It computes metrics including delta-v, thrust-to-weight, burn_time, and final_mass. Required features include mass data, propulsion specs, and environment settings. Optional features add gravity/atmosphere corrections, multi-stage delta-v, and data export. The tool also provides a compact SVG silhouette for quick reference.
Inputs & Outputs: Inputs are named, typed, and validated (mass in kg, Isp in s). Outputs include delta_v_m_s, thrust_to_weight, burn_time_s, final_mass_kg, payload_fraction, and an SVG reference. Algorithms & Calculations: Core calculation uses the Tsiolkovsky equation delta_v = Isp * g0 * ln(m0/mf), with m0 = dry_mass + propellant_mass + payload_mass, mf = dry_mass + payload_mass. Burn time approximations use propellant_mass and average thrust; atmosphere and gravity corrections apply simple factors. Error & Edge Cases: Validation checks reject negative or zero critical values; missing required inputs raise errors; if Isp <=0 or mass fractions are invalid, provide diagnostics and avoid calculations. Industry/Region & Localization: Uses SI units; default gravity g0 = 9.80665 m/s^2; no currency or locale-specific data; suitable for education and hobbyist simulations across regions. Assumptions & Exclusions: Assumes ideal rocket equation baseline; excludes full 3D dynamics, detailed aerodynamic losses, and professional mission planning); data export formats and 2D silhouette are simplified references only.

How to Use

  1. Provide inputs: enter vessel_mass_kg, dry_mass_kg, propellant_mass_kg, Isp_s, engine_thrust_kN, payload_mass_kg optional.
  2. Set environment: choose gravity_scale (0–
  3. and atmosphere flag.
  4. Run calculations: trigger calculation to obtain delta_v_m_s, TWR, burn_time_s.
  5. Review outputs: inspect delta-v, burn time, and thrust-to-weight; adjust design as needed.
  6. Export data or SVG: download CSV/JSON or view the 2D silhouette.
How to use vessel viewer ksp

Frequently Asked Questions

Find Quick Answers

What is delta-v and why does it matter?
Delta-v represents the velocity change a vessel can achieve with a given propellant mass and mass distribution. It informs mission feasibility, staging decisions, and maneuver planning by indicating how much propulsive capability remains after losses. It is a fundamental planning metric in spaceflight concepts.
What data is required to run calculations?
Essential inputs include dry mass, propellant mass, and specific impulse, plus engine thrust and payload mass if relevant. Without these, the core delta-v and related outputs cannot be computed reliably. Optional parameters refine gravity and atmosphere effects.
Can I evaluate multi-stage vessels?
Yes. Provide masses and Isp for each stage and the tool will incorporate stage masses into the mass budget. It can compute stage-by-stage delta-v or an overall delta-v, depending on the selected calculations, aiding design comparisons.
What units are used?
All inputs and outputs use SI units: masses in kilograms, thrust in kilonewtons, velocity in meters per second, and thrust-to-weight as a dimensionless ratio. Isp remains in seconds, with g0 defined as 9.80665 m/s^2.

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