On Thu, May 23, 2019 at 8:52 PM Monroe L. King Jr. <
monroe@xxxxxxxxxxxxxxxxxx> wrote:
You could use a jetpak for a landing that might be the only real useful
use of one lol (not really). 10 min wingsuit flight 5 min jetpak
landing.
If you're lazy you could use the jetpak to get you to the takeoff point
I guess too.
Stall speed is in the 60mph range could it be done? Probably with a nice
headwind and a belly pan strapped to your underside. lol don't screw up
though lol
That guy did not land in the water though it's just fake fake fake.
Monroe
-------- Original Message --------velocities,
Subject: [AR] Re: SpaceX Single Stage to Orbit
From: roxanna Mason <rocketmaster.ken@xxxxxxxxx>
Date: Thu, May 23, 2019 5:49 pm
To: arocket@xxxxxxxxxxxxx
What's the stall speed plus ground effect all help reduce impact trauma.
On Thu, May 23, 2019 at 5:02 AM Monroe L. King Jr. <
monroe@xxxxxxxxxxxxxxxxxx> wrote:
The Parachute is optional.
https://youtu.be/o2xmAWS4akE?t=100
FAKE lol so fake.
-------- Original Message --------
Subject: [AR] Re: SpaceX Single Stage to Orbit
From: Craig Fink <webegood@xxxxxxxxx>
Date: Wed, May 22, 2019 7:01 pm
To: arocket@xxxxxxxxxxxxx
Hydrogen tanks have better crumple zones and lower terminal
ground.but
I still think you should consider having a reserve parachute. With awrote:
properly designed entry suit you should be able to eject anywhere!
The Parachute is optional.
https://youtu.be/o2xmAWS4akE?t=100
On Wed, May 22, 2019 at 11:05 AM David Summers <dvidsum@xxxxxxxxx>
Oh, I don't know, it will probably reach rest with respect to
wrote:With
wclaybaugh2@xxxxxxxxx>a good enough crash couch might even be survivable!
On Wed, May 22, 2019, 12:58 PM William Claybaugh <
reentry.wrote:
Craig:
There is not enough mass reserve on this vehicle to land it after
Bill
On Wed, 22 May 2019 at 07:24, Craig Fink <webegood@xxxxxxxxx>
onlystage.
Bill,
Landing Propellant mass fraction used for delta-V should be
significantly less for this prototype than for the Falcon 9 first
The Fly-Back Burn and the Entry Burn are unnecessary, so it's
Velocitynecessary to have enough delta-V to slow down from Terminal
land.to
wclaybaugh2@xxxxxxxxx>zero at the ground.
On Wed, May 22, 2019 at 8:51 AM William Claybaugh <
wrote:
Not fully reusable; there will not be sufficient propellant to
are
Time will tell as SpaceX is walking down a flexible path, they
I'veapparently taking two paths right now, to their goal. From what
flyingseen
controlso far, the landing legs are an integral part of the aerodynamic
surfaces so probably wouldn't be taken off. Like an aircraft
foracross
Pacific, one would not expect the aircraft to carry enough fuel
placethe
return trip. For a Launch Vehicle, the Destination is LEO, a
Refuelto let
passengers and cargo off, take on new passenger and cargo and
Orbitfor
vehicle. Whenthe return trip. Refueling in LEO is already a goal for this
wrote:refueling is added to the Prototype? Time will tell.
Bill
On Wed, 22 May 2019 at 05:47, Craig Fink <webegood@xxxxxxxxx>
Looks like we are close to seeing the first Single Stage to
researchvehicle, capablelaunch. As a bonus, this launch should be a fully reusable
step on theof Entry and Landing. Plus, this accomplishment will be just a
path to his new launch vehicle, as the SSTO is SpaceX's
SpaceXversion of
Starship's second stage.
https://youtu.be/6IydYEBrk0E?t=413
CloudLicker on Youtube seems to do a good job aggregating
News
1960s.so you don't have to.
Following SpaceX today is what following NASA was like in the
All Doing, less Talk. Exciting times ahead.--
Craig Fink
WeBeGood@xxxxxxxxx
--
Craig Fink
WeBeGood@xxxxxxxxx
--
Craig Fink
WeBeGood@xxxxxxxxx