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Conceptual design of a hypervelocity asteroid intercept vehicle (haiv) flight validation mission
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Getzandanner, Kenneth Steiner, Mark Barbee, Brent W. Wie, Bong |
| Copyright Year | 2013 |
| Description | In this paper we present a detailed overview of the MDL study results and subsequent advances in the design of GNC algorithms for accurate terminal guidance during hypervelocity NEO intercept. The MDL study produced a conceptual con guration of the two-body HAIV and its subsystems; a mission scenario and trajectory design for a notional flight validation mission to a selected candidate target NEO; GNC results regarding the ability of the HAIV to reliably intercept small (50 m) NEOs at hypervelocity (typically greater than 10 km/s); candidate launch vehicle selection; a notional operations concept and cost estimate for the flight validation mission; and a list of topics to address during the remainder of our NIAC Phase II study. |
| File Size | 3939471 |
| Page Count | 4 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20130013405 |
| Archival Resource Key | ark:/13960/t8pc8097f |
| Language | English |
| Publisher Date | 2013-08-19 |
| Access Restriction | Open |
| Subject Keyword | Astronomy Terminal Guidance Algorithms Launch Vehicles Hypervelocity Projectiles Asteroids Near Earth Objects Mission Planning Interception Computerized Simulation Spacecraft Design Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
