1965 SARSA Summary

Program Units Safety Factor
1. Orbital Satellite 0 96%
2. Interplanetary Satellite 0 92%
3. Lunar Probe 0 86%
A. One Stage Rocket 0 85%
C. Three Stage Rocket 1 98%
EVA Suits n/a 81%
d. Two Person Lunar Module 1 36%
f. Three Person Capsule 1 91%
Photo-Reconnaissance n/a 80%

Earth based mission control allows, one time, a re-roll of a single failed safety check.

1 Launch Facility at an undisclosed location

1 Launch planned for 1966


Last updated: September 5, 2017 at 14:17 pm

Comments: 0

Comments are closed.