PROTOCOL // APOLLO-13

The Cardboard Adapter

A geometric and chemical specification for the CO₂ scrubber interface improvised aboard Apollo 13.

Saturn V rocket engines at Kennedy Space Center

Mission Brief

Date: April 11–17, 1970
Crew: Lovell, Swigert, Haise
Failure Mode: Oxygen Tank 2 explosion, forcing abandonment of Lunar Module ascent.
Critical Constraint: Square lithium hydroxide canisters (Command Module) incompatible with round ports (Lunar Module).

Source: Wikidata Q182252

I. Geometric Specification

The adapter solved a dimensional mismatch between two systems designed for different vessels. The solution required three components: a coupling sleeve, a flow distributor, and a seal.

Component Material Dimensions Tolerance
Canister Sleeve PVC Pipe Segment ID: 7.6 cm (3") ±0.5 mm
Flow Interface Plastic Bag (Polyethylene) Diameter: 15.2 cm N/A (Flexible)
Sealant Suit Gloves + Magazine Pages Thickness: 1.2 mm Compression Fit
Strut Assembly Cardboard Flight Manual Covers Length: 20.3 cm Rigid Fold

II. Chemical Stoichiometry

The adapter was merely the conduit; the reaction was the salvation. Lithium hydroxide scrubbed carbon dioxide from the cabin atmosphere via irreversible precipitation.

2 LiOH(s) + CO₂(g) ⟶ Li₂CO₃(s) + H₂O(l)

III. Verification Protocol

Ground control simulated the construction using identical materials. The flight manual covers provided structural rigidity; the plastic bag ensured gas permeability while maintaining pressure differential.

Result: Successful integration. The adapter reduced cabin CO₂ levels from lethal 7,000 ppm to safe operating range within 4 hours.