Trade Study Manager Skill
Read
CONVENTIONS.mdat the repo root before proceeding.
This skill supports the decision-making that happens before detailed analysis — choosing between mission architectures, subsystem approaches, or technology options using structured trade methodology.
Before You Begin
Ask the user (if not already known):
- What decision needs to be made? (orbit selection, propulsion type, power source, payload selection, launch vehicle, constellation vs single, etc.)
- What are the candidate options? (at least 2, ideally 3-5)
- Who are the stakeholders? (engineering, science, management, cost — each may weight criteria differently)
- What is the decision deadline / review gate? (SRR, PDR, mission proposal)
- What design phase?
Applicable Phases
- Primary: Phase A (architecture selection — this is when most trades happen)
- Supporting: Phase B (detailed subsystem trades), Phase C (change impact assessment)
Trade Study Methodology
1. Define the Trade Space
- List candidate options with a brief description of each.
- Define the "do nothing" or "baseline" option if applicable.
- Eliminate clearly infeasible options early (with documented rationale).
2. Define Evaluation Criteria (Figures of Merit)
Common criteria for space missions:
- Performance: Resolution, data rate, coverage, revisit time
- Mass: Total system mass (lighter = more launch margin or smaller LV)
- Power: Total power demand vs. available
- Cost: Development cost, operations cost, launch cost
- Risk: Technical maturity (TRL), schedule risk, supply chain
- Heritage: Flight-proven vs. novel
- Operability: Ground station needs, autonomous capability, complexity
- Lifetime: Degradation, consumables, reliability
3. Weight the Criteria
- Use pairwise comparison (AHP) or direct assignment.
- Weights must sum to 1.0 (or 100%).
- Document the rationale for weighting — this is often the most debated step.
4. Score the Options
- Score each option against each criterion (typically 1-5 or 1-10 scale).
- Scoring rules: Define what each score means before scoring (e.g., "5 = exceeds requirement with margin, 3 = meets requirement, 1 = does not meet").
- Score independently before group discussion to avoid groupthink.
5. Calculate Weighted Scores
$S_{option} = \sum_{i} w_i \times s_i$
6. Sensitivity Analysis
- Vary the weights ±20% and see if the winner changes.
- Identify which criteria are "swing factors" — small weight changes flip the result.
- If the trade is sensitive, the decision needs more analysis before commitment.
Trade Matrix Format
| Criterion | Weight | Option A | Score | Option B | Score | Option C | Score | |:---|:---|:---|:---|:---|:---|:---|:---| | Performance | 0.30 | Excellent | 5 | Good | 3 | Good | 3 | | Mass | 0.20 | 85 kg | 4 | 120 kg | 2 | 95 kg | 3 | | Cost | 0.25 | $15M | 3 | $8M | 5 | $12M | 4 | | Risk (TRL) | 0.15 | TRL 6 | 3 | TRL 9 | 5 | TRL 4 | 2 | | Heritage | 0.10 | Partial | 3 | Full | 5 | None | 1 | | Weighted Total | — | — | 3.70 | — | 3.70 | — | 2.85 |
Common Space Mission Trades
Reference trades that come up repeatedly:
- Orbit: LEO (low latency, high drag) vs. MEO vs. GEO (large coverage, high delta-v, radiation)
- Propulsion: Chemical (simple, high thrust) vs. Electric (efficient, slow) vs. Cold gas (simple, low performance)
- Power: Solar (common, distance-limited) vs. RTG (deep space, regulatory) vs. Battery-only (short missions)
- Constellation: Single high-capability vs. distributed lower-capability (coverage vs. cost)
- Launch vehicle: Rideshare (cheap, constrained orbit) vs. Dedicated (expensive, flexible)
Output Format
- Trade Study Report (
trade_report.md): Decision question, options, criteria, weights, scoring matrix, sensitivity analysis, and recommendation with rationale. - Decision Record: One-paragraph summary capturing: "We chose [Option X] because [key reasons], accepting [trade-offs]."
Interface
- Reads from:
/requirements/(mission objectives and constraints), any existing/analysis/outputs that inform the trade - Writes to:
/analysis/trade-study-manager/ - Consumed by: All downstream skills (the trade decision shapes the entire mission architecture)
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