'Launch configuration' diaporamas de présentation

Parallelizing and Optimizing Programs for GPU Acceleration using CUDA

Parallelizing and Optimizing Programs for GPU Acceleration using CUDA. Martin Burtscher Department of Computer Science. CUDA Optimization Tutorial. Martin Burtscher burtscher@txstate.edu http://www.cs.txstate.edu/~burtscher/ Tutorial slides

1.28k views • 113 slides

CanSat 20 20 Preliminary Design Review (PDR) Outline Version 1. 0

CanSat 20 20 Preliminary Design Review (PDR) Outline Version 1. 0. Your Team # Here Your Team Name Here. Presentation Outline. Provide a simple outline of the presentation I ndicate the team member(s) who will be presenting each section Terms:

962 views • 95 slides

L1 and L2 Observatories in the Post-2010 Era

322 views • 24 slides

Human Exploration of the Moon and Mars

Human Exploration of the Moon and Mars. Launch configuration. Crew Exploration Vehicle. Service module carries the CEV to the Moon. Lunar Surface Module. Site Selection for Moon. Optimal Science Base. * Numbers indicate sortie sites. 58. 31. 27. 49. 41. 18. 38. 10. 6. 57. 50.

531 views • 24 slides

Human Exploration of the Moon and Mars

Human Exploration of the Moon and Mars. Launch configuration. Crew Exploration Vehicle. Service module carries the CEV to the Moon. Lunar Surface Module. Site Selection for Moon. Optimal Science Base. * Numbers indicate sortie sites. 58. 31. 27. 49. 41. 18. 38. 10. 6. 57. 50.

332 views • 24 slides

X-ray Wide Field Imager

305 views • 18 slides

Mission Design Dave Curtis UCB/SSL Space Sciences Laboratory University of California, Berkeley

Mission Design Dave Curtis UCB/SSL Space Sciences Laboratory University of California, Berkeley. Mission Design Agenda. AGENDA Launch Configuration Early Orbit Commissioning Science Operations Issues. Launch Configuration. Launch configuration constrained by:

104 views • 10 slides

ESTREMO/WXT Initiative: AAS-I Contribution

ESTREMO/WXT Initiative: AAS-I Contribution. ESTREMO/WXT: Preliminary Consideration. For preliminary ESTREMO feasibility evaluation the basic consideration are about: Launch capability (mass, firing volume, firing height) of Vega for LEO Payload Accommodation Fast pointing

177 views • 8 slides