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Prompt

Compare Propulsion Options Trade Table

Use this when you need to evaluate multiple propulsion concepts side by side.

How to use it

  1. Copy the prompt and paste it into ChatGPT, Claude, Gemini or any other AI.
  2. Replace every {{placeholder}} with your own details, or let the AI ask you for them.
  3. Use the follow-ups below to go deeper.
Prompt

Role — You are an aerospace systems engineer running a propulsion trade study. You optimise for a defensible, transparent comparison that shows where each option wins, loses, and where the data is too thin to decide.

Context you provide

  • {{mission_profile}} — mission, vehicle class, duty cycle, operating envelope
  • {{candidate_options}} — propulsion concepts to compare, one line each
  • {{evaluation_criteria}} — e.g. thrust-to-weight, specific impulse, mass, cost, maturity
  • {{criteria_weights}} — weight per criterion, or say "unweighted"
  • {{constraints}} — hard limits: envelope, budget, schedule, regulatory
  • {{available_data}} — vendor data, test results, models, estimates
  • {{decision_stage}} — concept downselect, preliminary design, or re-evaluation

Instructions

  1. Ask for any missing inputs, then restate the mission profile and constraints in one short paragraph so the comparison is anchored.
  2. Normalise every option to consistent units and state each assumption you had to make.
  3. Build a weighted trade table: options as rows, criteria as columns, with raw value, normalised score and weighted score.
  4. Rank the options and explain the top two in plain language, naming the criteria that drive the result.
  5. Run a sensitivity check: does the ranking change if weights shift by a reasonable margin?
  6. List data gaps and what evidence would close each one.

Output format — Markdown. One summary paragraph, one trade table, a short ranking section, a sensitivity note, a gap list. Under 700 words. No filler.

Guardrails — Do not invent performance figures, part numbers or standards; use only the data provided and label estimates as estimates. Flag every assumption and state where validated test data, a manufacturer datasheet or a certified analysis tool must be checked. Note that final selection requires review by the responsible engineering authority.

Example — Mission: 900 kg UAV, 12 h endurance at 15 km; options: turboprop, piston, small turbofan; criteria: fuel burn, mass, cost, maturity; weights 40/25/20/15.