The foundational misunderstanding behind it seems to be that they
think "terminal buoyant velocity" for it is extremely fast.
They cite supersonic ping ball cannons as the proof of concept that
shows they can build a scramjet.
http://www.carpeastra.co.uk/showpage.php?pageName=04_proof
Also, "The above proof shows that the theoretical maximum Isp of
burning H2 in air when the launch vehicle is displacing its own weight
in air should be approximately 80,000 seconds at around Mach 5 and
under the same conditions"
On Tue, May 7, 2019 at 10:08 PM Troy Prideaux
<troy@xxxxxxxxxxxxxxxxxxxxx> wrote:
Not much mention on how they deal with aero drag.
From: arocket-bounce@xxxxxxxxxxxxx [mailto:arocket-bounce@xxxxxxxxxxxxx] On ;
Behalf Of Doug Jones (Redacted sender "randome" for DMARC)
Sent: Wednesday, 8 May 2019 2:41 PM
To: arocket@xxxxxxxxxxxxx
Subject: [AR] Re: RAROSS
Not just vaporware, but lighter than air vaporware! Profit!
On 2019-05-07 7:22 PM, Ben Brockert wrote:
Self-licking rockoon.
https://www.youtube.com/watch?v=Wpwog0UguJA
http://www.carpeastra.co.uk/showpage.php?pageName=03_concepts
