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A suborbital abort guidance scheme for orbital returns to the launch site
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lacy, W. R. |
| Copyright Year | 1971 |
| Description | A suborbital abort guidance scheme is presented for returning the orbiter vehicle to the launch site in the event of a booster malfunction. The guidance scheme described, referred to as FBGUID, represents a simple closed-form technique to the flyback abort problem. In addition to returning to the launch site, objectives of the formulation are to preclude excessive structural and heating loads. A demonstration of the feasibility of this abort guidance concept is included for a 150-second abort time. |
| File Size | 1220558 |
| Page Count | 52 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720006189 |
| Archival Resource Key | ark:/13960/t7jq5qt84 |
| Language | English |
| Publisher Date | 1971-06-30 |
| Access Restriction | Open |
| Subject Keyword | Space Sciences Malfunctions Engine Failure Spacecraft Guidance Mission Planning Aborted Missions Abort Trajectories Spacecraft Launching Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
