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Ultimate Saturn V Quiz - Statistics
General Stats
- This quiz has been taken 26 times
- The average score is 11 of 38
Answer Stats
| Hint | Answer | % Correct |
|---|---|---|
| Number of stages | 3 | 100%
|
| Number of Crew | 3 | 100%
|
| Associated Program: | Apollo | 88%
|
| Total launched Saturn V's | 13 | 71%
|
| Acronym: LM | Lunar Module | 65%
|
| Number of engines on S-IC and S-II | 5 | 59%
|
| Formal designation for Stage 1 | S-IC | 53%
|
| Formal designation for Stage 2 | S-II | 53%
|
| Formal designation for Stage 3 | S-IVB | 53%
|
| Manufacturer of the S-IC stage | Boeing | 47%
|
| Acronym: CSM | Command and Service Module | 41%
|
| Engines employed on S-IC | F-1 | 41%
|
| Acronym: LES | Launch Escape System | 41%
|
| Acronym: VAB | Vehicle Assembly Building | 41%
|
| Engines employed on the S-II | J-2 | 29%
|
| Engines employed on the S-IVB | J-2 | 29%
|
| Fuel of the F-1 Engine | RP-1 | 29%
|
| Which S-IC engine ignited first | Center | 24%
|
| Manufacture of the Saturn V instrument unit | IBM | 24%
|
| Fuel of the S-II Engines | LH2 | 24%
|
| Name of the only manned Non-Apollo mission the Saturn V performed | Skylab 1 | 18%
|
| Category of Launch Vehicle | Super Heavy | 18%
|
| Manufacturer of the S-II stage | North American Aviation | 12%
|
| Name of motors used to settle propellant prior to S-II ignition | Ullage | 12%
|
| Length of the TLI injection burn | 6 minutes | 6%
|
| Fate of S-IVB after Apollo 13 | Crashed into the moon | 6%
|
| Manufacturer of the S-IVB stage | Douglas Aircraft Company | 6%
|
| Abort mode in which the S-IVB and CM engine would be used during an S-II failure | S-IVB to COI | 6%
|
| Time of S-IC ignition (notated in T-) | T-9 | 6%
|
| Altitude of which the final parking orbit never exceeded (in km) | 190 | 0%
|
| Device deployed during Abort Mode IB | Canards | 0%
|
| Acronym: COI | Contingency Orbit Insertion | 0%
|
| Lunar mission configuration | Earth Orbit Rendezvous | 0%
|
| Event which concludes Abort Mode IC | LES seperation | 0%
|
| Phenomenon that necessitated the center S-II engine shutting down | Longitudinal Pogo Oscillations | 0%
|
| Abort mode in which only the S-IVB engine would be used during an S-II failure | S-IVB to Orbit | 0%
|
| Time that concludes Abort Mode IA (notated in T+) | T+42 | 0%
|
| Manuever done to extract the Lunar Module | Transposition, Docking, Extraction | 0%
|
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