File:Dragon Pad Abort Test.jpg
From Infogalactic: the planetary knowledge core
Size of this preview: 800 × 535 pixels. Other resolutions: 320 × 214 pixels | 3,000 × 2,008 pixels.
Original file (3,000 × 2,008 pixels, file size: 1 MB, MIME type: image/jpeg)
Summary
Eight SuperDraco engines boost a SpaceX Crew Dragon spacecraft away from Space Launch Complex 40 at Cape Canaveral Air Force Station in an emergency pad abort simulation. Each of the eight SuperDraco engine generates 15,000 pounds of thrust and burns about six seconds. The test began at 9 a.m. After the engines shut down, the Dragon spacecraft's trunk, with passive fins for stability, will separate when it reaches peak altitude.
Licensing
Lua error in package.lua at line 80: module 'strict' not found.
File history
Click on a date/time to view the file as it appeared at that time.
Date/Time | Thumbnail | Dimensions | User | Comment | |
---|---|---|---|---|---|
current | 20:15, 7 January 2017 | 3,000 × 2,008 (1 MB) | 127.0.0.1 (talk) | Eight SuperDraco engines boost a SpaceX Crew Dragon spacecraft away from Space Launch Complex 40 at Cape Canaveral Air Force Station in an emergency pad abort simulation. Each of the eight SuperDraco engine generates 15,000 pounds of thrust and burns about six seconds. The test began at 9 a.m. After the engines shut down, the Dragon spacecraft's trunk, with passive fins for stability, will separate when it reaches peak altitude. |
- You cannot overwrite this file.
File usage
The following page links to this file: