On Monday, May 29, 2017 at 2:13:48 PM UTC+12, Jeff Findley wrote:
> In article <
939fb6e3-b1fa-4bf7...@googlegroups.com>,
>
mokme...@gmail.com says...
> >
> > On Monday, May 29, 2017 at 2:05:18 AM UTC+12, Jeff Findley wrote:
> > >
> > > I'm surprised they got as far as they did.
> > >
> > > But yes, there is a bit of a PR spin going on in the news articles.
> > > This was a test flight and it was mostly successful... mostly. But it
> > > did not go into orbit, so it's not quite ready for paying customers who
> > > expect their satellite to be placed into earth orbit.
> > >
> > > Still, SpaceX had several Falcon 1 failures before they finally "got it
> > > right". This stuff isn't easy.
> >
> > Jeff,
> >
> > RocketLab received $75 million a few months ago, and announced
> > three TEST FLIGHT prior to committing to their first COMMERCIAL
> > LAUNCH.
>
> Yes, this has been reported.
>
> > Had everything gone perfectly, the company may have dropped one
> > test launch. As it stands, they will review 25,000 channels of
> > data collected,
>
> Yes that 25,000 channels of data collected has been reported too.
>
> > and run it through their automated design and production process.
>
> You make it sound like Rocket Lab has some sort of artificial
> intelligence that can take 25,000 channels of data from a test launch
> and tweak the production process without human intervention.
You make shit up and then gripe about what you make up. lol. What I said is true. What you said. Not so much.
>That
> simply isn't true though.
The part you made up isn't true. I agree.
> That data will be interpreted by engineers,
Of course, with assistance from computers. You're the one who made up shit about no human intervention. OF COURSE their engineers will review everything.
> not by some "automated design and production process".
You haven't done much engineering for production recently have you? lol. Production tools have become highly automated over the past few years.
> > Their tooling is largely digitally defined, and they have an
> > awesome system of continuous improvement building their hardware
> > with equipment that others might have called in an earlier day
> > rapid prototyping. Their next rocket will have some awesome
> > improvements, and their next one after that. As they strive
> > and achieve perfection.
>
> I'll wait to see how the next couple of launches go.
Quite right! They planned three test launches, and intend to take advantage of all three to exercise their system before going to their commercial campaigns. Observers will be surprised by the rapidity of the process. A Delta campaign takes years. A RocketLab campaign will take weeks.
> Like I said, this
> stuff isn't easy.
True, but its getting easier.
http://www.ulalaunch.com/uploads/docs/Published_Papers/Evolution/AIAA11731CriticalEventsDIV.pdf
United Launch Alliance points out that the Delta IV has a 40 year history, and to create the EELV and Delta Heavy it took $60 billion and 30 years leading up to that point.
SpaceX took 15 years and $10 billion to achieve what they have.
RocketLab took 4 years and $100 million.
True, 150 kg to SSO is not 53,000 kg - but Electron places 250 kg into Low inclination orbits from their Kennedy Space Center launch site, and its good to remember that the original Thor Delta put up only 226 kg back in the day.
configured as a common core booster, with two liquid fuelled strap-ons, operating as an additional stage, payload of 625 kg is achieved. Adding four liquid fuelled strap-ons as another added stage, increases payload capacity to 1,625 kg!
Without major tooling changes AT ALL.
> Running out of money before successfully making orbit
> has happened to other start-ups in the past.
True of any business.
> It could happen again,
With RocketLab's launch book and capabilities, it is unlikely to happen to them.
> even though I hope it doesn't.
Yeah, I can feel the love! lol.
>
> Jeff
> --
> All opinions posted by me on Usenet News are mine, and mine alone.
> These posts do not reflect the opinions of my family, friends,
> employer, or any organization that I am a member of.
PILOTED ELECTRON
A biosuit with built in thermal protection allows the two stage Electron to send an astronaut on the flying suit ride of their life!
https://www.youtube.com/watch?v=7f-K-XnHi9I
https://www.youtube.com/watch?v=Qnv664BmdPU
Sky dive from space!
The 1 meter diameter main body of the Electron is large enough to support a BD-5 cockpit - and aircraft.
https://www.the-blueprints.com/blueprints-depot-restricted/modernplanes/modern-ba-bn/bd_5b-32725.jpg
A BD-5J masses 161 kg and is 4 meters long and has a 0.61 meter wide cabin.
Lightweight structural aerogels are available.
https://www.youtube.com/watch?v=k8OhJKR3AA4
From which to make DynaSoar X-20 subscale lightweight version
http://www.astronautix.com/graphics/x/x20titn1.jpg
http://www.aerospaceprojectsreview.com/blog/wp-content/uploads/2012/01/Martin-3-view1.gif
A 40% scale model of the DynaSoar X-20 would have the same cabin volume as the BD-5J.
The mass of the sub-scale version 262 kg when made of the same materials as the original X-20, which weighs 4,091 kg when full size.
When constructed of advanced materials, weights are cut to 125 kg, without pilot and consumables. The smaller version has a 2.4 meter wingspan.
An 'Electron-Heavy' - can't be called Proton that name is already taken! - lol places this lightweight sub scale X-20 derivative carrying one pilot, into orbit.
Another 625 kg stage, launched previously, is equipped with a solar ion booster rocket, and a rocket belt. The DynaSoar docks with the booster stage and both vehicles are accelerated to lunar insertion trajectory. The booster brings the vehicle to a low lunar orbit four days later. The astronaut, moves from the DynaSoar to the rocket belt, and lands on the moon, leaving the equipment on orbit. The astronaut then returns stowing all away, and boosting back to Earth. The booster and spacecraft separate, and re-enter landing back at the launch center to be refurbished and reused.