A geometric and chemical specification for the CO₂ scrubber interface improvised aboard Apollo 13.
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).
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 |
The adapter was merely the conduit; the reaction was the salvation. Lithium hydroxide scrubbed carbon dioxide from the cabin atmosphere via irreversible precipitation.
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.