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Jannaf lessons learned panel discussion
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Richards, Steve |
| Copyright Year | 2010 |
| Description | The difference between the AS-510 observed and predicted separation distance is attributed to a greater F-1 engine "tail off" impulse than that used in the separation distance prediction. . The F-1 thrust decay was normal and not appreciably different from previous (AS-505 through 509) flights. . Analysis indicates that with an S-IC stage having only four retro motors, failure of one retro motor to ignite would result in marginal separation distances and, in the 3-sigma case, re-contact of the two stages. . S-IC-11 and subsequent flight stages were equipped with eight retro motors rather than the planned four. |
| File Size | 1241609 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20100023317 |
| Archival Resource Key | ark:/13960/t58d4wn7z |
| Language | English |
| Publisher Date | 2010-05-03 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Stage Separation Lessons Learned Impulses Costs Ignition Propulsion Aerodynamic Forces Distance Thrust Failure Payloads Pneumatics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |
