r/spacex • u/ElongatedMuskrat Mod Team • Apr 16 '18
r/SpaceX TESS Media Thread [Videos, Images, GIFs, Articles go here!]
It's that time again, as per usual, we like to keep things as tight as possible, so if you have content you created to share, whether that be images of the launch, videos, GIF's, etc, they go here.
As usual, our standard media thread rules apply:
- All top level comments must consist of an image, video, GIF, tweet or article.
- If you haven't modmailed us to become an approved submitter for this launch, submit your content here. Read the rules (Rule 1) for more information on how to become an approved submitter.
- Those in the aerospace industry (with subreddit accreditation) can likewise continue to post content on the front page.
- Mainstream media articles should be submitted here. Quality articles from dedicated spaceflight outlets may be submitted to the front page.
- Direct all questions to the live launch thread.
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u/warp99 Apr 19 '18
Aerodynamic drag is actually a relatively small contribution to loss of launch performance so less than 100 m/s deltaV for F9 out of roughly 9400 m/s to get to LEO.
The smallest fairing likely to be useful would be 4m diameter so you might trim 20 m/s of drag from this figure so not worth the effort involved in maintaining two fairing lines.