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Computer program trajectory optimization by explicit numerical methods
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1966 |
| Description | Computer program using numerical methods that calculates minimum time for space vehicle to meet its mission with optimum trajectory, and can maximize option if burning time is fixed |
| File Size | 2234725 |
| Page Count | 96 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19670008304 |
| Archival Resource Key | ark:/13960/t1mh2c12j |
| Language | English |
| Publisher Date | 1966-12-08 |
| Access Restriction | Open |
| Subject Keyword | Computer Program Numerical Integration Trajectory Optimization Burning Rate Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |