Which cognitive biases were evident in NASA / Lockheed Martin's collapse?

5 bias patterns are documented in this case, led by Cognitive Misering. The full set: Cognitive Misering, Confirmation Bias, Groupthink, Hindsight Bias, Status Quo Bias. Each is mapped to Decision Intel's 22-bias R²F taxonomy with stable IDs and academic citations.

Did these cognitive biases cause NASA / Lockheed Martin's collapse?

Decision Intel identifies reasoning-risk indicators correlated with poor outcomes — it does not claim to establish causation. That honesty is the procurement weapon: a CSO can defend a score that names the risk indicators a committee should pressure-test, not one that pretends to prove the cause. Cognitive Misering and the other documented patterns were detectable in the reasoning before the outcome was known; whether they caused it is a question no audit can settle — too many other factors (market, timing, execution) are in play. A reasoning audit names the risk indicators a committee should pressure-test, not a verdict it should accept.

What is Decision Intel's reasoning audit?

Decision Intel runs a Recognition-Rigor Framework (R²F) audit on strategic memos, detecting cognitive biases from a 22-bias canonical taxonomy and producing a Decision Quality Index (DQI) score. The audit produces a hashed, tamper-evident Decision Provenance Record (DPR) suitable for audit-committee review.

All case studies

Catastrophic failureAerospace1999

NASA / Lockheed Martin

Mars Climate Orbiter Unit Conversion Failure

Estimated impact: $125M spacecraft destroyed

F14

Decision Quality Index (simulated)

Critical · 5 biases detected, 2 toxic combinations

The $125M Mars Climate Orbiter was destroyed when it entered Mars' atmosphere at too low an altitude. The root cause was a unit mismatch: Lockheed Martin's software output thrust data in pound-force-seconds while NASA's navigation software expected newton-seconds.

Decision context

Whether NASA's verification and validation process should have caught the unit mismatch during the 9-month cruise phase, during which trajectory deviations were observed but attributed to other causes.

Deep hindsight-stripped analysis coming soon. This case is part of our ongoing backfill to reconstruct what was flaggable in the record at decision time. The summary and bias profile below are drawn from primary sources.

Decision anatomy

Monetary stakes

High

Dissent suppressed

Time pressure

Present

Unanimous consensus

Decision participants

Dissent encouraged

External advisors

Iterative process

Red = risk factor present · Green = protective factor present

Biases present in the decision

★Cognitive Misering

critical

Confirmation Bias

high

Groupthink

high

Hindsight Bias

medium

Status Quo Bias

medium

★ Primary driver · Severity estimated from bias type and decision outcome

3D Decision Knowledge Graph

NASA / Lockheed Martin · 5 biases, 2 toxic combinations

Drag to rotate · Scroll to zoom · Click to explore

Decision

Critical

High

Medium

Toxic

Bias Intensity Profile

Severity × confidence across 5 detected biases

Toxic combinations

!Status Quo Lock

Loss aversion combined with status quo bias makes even clearly beneficial change feel impossible.

!Echo Chamber

Group members reinforce each other's views, systematically filtering out dissenting signals.

The curated library this case sits in

Across all 155 curated case studies in our library, by documented outcome:

123

documented failures

partial / mixed

documented successes

The library is curated toward documented failures, so this split describes the library, not the base rate of deals. The case above is one row in it.

■ Failure■ Partial■ Success

Lessons learned

Cognitive misering: trajectory deviations during the cruise phase were observed but corrected without investigating root cause
Confirmation bias: engineers assumed the navigation model was correct and attributed discrepancies to solar radiation pressure
Interface specification reviews between contractors and NASA were insufficient — unit conventions were not explicitly verified

Source: NASA Mars Climate Orbiter Mishap Investigation Board Phase I Report (1999) (Post Mortem)

Pilot slots available

These patterns were flaggable in NASA / Lockheed Martin's own record — before the outcome.

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Workflows that fire on decisions like NASA / Lockheed Martin’s

The same Recognition-Rigor Framework that documents this case audits memos in the same shape — before the outcome forces the lesson.

For CSOs and Heads of Strategic Planning

Strategic memo audit

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Decision pre-mortem

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All case studies

Catastrophic failureAerospace1999

NASA / Lockheed Martin

Mars Climate Orbiter Unit Conversion Failure

Estimated impact: $125M spacecraft destroyed

F14

Decision Quality Index (simulated)

Critical · 5 biases detected, 2 toxic combinations

Decision context

Decision anatomy

Monetary stakes

High

Dissent suppressed

Time pressure

Present

Unanimous consensus

Decision participants

Dissent encouraged

External advisors

Iterative process

Red = risk factor present · Green = protective factor present

Biases present in the decision

★Cognitive Misering

critical

Confirmation Bias

high

Groupthink

high

Hindsight Bias

medium

Status Quo Bias

medium

★ Primary driver · Severity estimated from bias type and decision outcome

3D Decision Knowledge Graph

NASA / Lockheed Martin · 5 biases, 2 toxic combinations

Drag to rotate · Scroll to zoom · Click to explore

Decision

Critical

High

Medium

Toxic

Bias Intensity Profile

Severity × confidence across 5 detected biases

Toxic combinations

!Status Quo Lock

Loss aversion combined with status quo bias makes even clearly beneficial change feel impossible.

!Echo Chamber

Group members reinforce each other's views, systematically filtering out dissenting signals.

The curated library this case sits in

Across all 155 curated case studies in our library, by documented outcome:

123

documented failures

partial / mixed

documented successes

The library is curated toward documented failures, so this split describes the library, not the base rate of deals. The case above is one row in it.

■ Failure■ Partial■ Success

Lessons learned

Cognitive misering: trajectory deviations during the cruise phase were observed but corrected without investigating root cause
Confirmation bias: engineers assumed the navigation model was correct and attributed discrepancies to solar radiation pressure
Interface specification reviews between contractors and NASA were insufficient — unit conventions were not explicitly verified

Source: NASA Mars Climate Orbiter Mishap Investigation Board Phase I Report (1999) (Post Mortem)

Pilot slots available