Author Topic: Dawn Aerospace  (Read 84170 times)

Offline FutureSpaceTourist

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Dawn Aerospace
« on: 09/01/2021 07:47 am »
Couldn’t find a thread for: https://www.dawnaerospace.com/

They are working on reusable spaceplanes. The Mk II Aurora is suborbital and has begun flight (not yet rocket flight) test. The planned Mk III is a small sat launcher.
Media report on current testing:

https://newatlas.com/space/dawn-aerospace-aurora-reusable-spaceplane-demonstrator-test-flights/

Quote
Reusable spaceplane demonstrator completes 5 test flights in 3 days

By David Szondy
August 31, 2021

Dawn Aerospace has successfully completed five test flights of its uncrewed Mk-II Aurora suborbital spaceplane in the skies over Glentanner Aerodrome on New Zealand’s South Island. The flights were conducted by the New Zealand-Dutch space transportation company from July 28 to 30, 2021 at altitudes of up to 3,400 feet (1,036 m), with the prototype airframe fitted with surrogate jet engines.

P.S. First 2 attachments are fine when opened, don’t know why they’re black in preview :(
« Last Edit: 09/01/2021 07:48 am by FutureSpaceTourist »

Offline FutureSpaceTourist

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Re: Dawn Aerospace
« Reply #1 on: 09/01/2021 07:51 am »
Some YT videos






Offline jdon759

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Re: Dawn Aerospace
« Reply #2 on: 09/01/2021 09:21 am »
I'm not sure this thread should be in commercial crew vehicles...

Yay!  I quite like Dawn.  They used to have a pretty unique plan for their rockets: selling orbital downmass rather than upmass.  Unfortunately, it looks like in the last ~11 months since I checked their progress, they've done away with that plan  :'( .  But that does nothing to reduce the elegant appearance of their suborbital rocket & (now 2-stage) launcher.
« Last Edit: 09/01/2021 09:22 am by jdon759 »
Where would we be today if our forefathers hadn't dreamt of where they'd be tomorrow?  (For better and worse)

Offline FutureSpaceTourist

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Re: Dawn Aerospace
« Reply #3 on: 09/06/2021 08:45 am »

Offline TrevorMonty

Re: Dawn Aerospace
« Reply #4 on: 09/06/2021 09:49 am »

Mark 2 engine test.

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Offline TrevorMonty

Re: Dawn Aerospace
« Reply #5 on: 08/16/2022 09:47 am »
Dawn have been busy landing Rocket Powered space planes and sell small in space thrusters.

https://twitter.com/DawnAerospace?t=hf5SNfl0U2kgXgbAXpnK1g&s=09
« Last Edit: 08/17/2022 08:31 am by zubenelgenubi »

Offline Rik ISS-fan

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Re: Dawn Aerospace
« Reply #6 on: 08/20/2022 01:57 pm »
Finally some other NSF member got aware of Dawn Aerospace and started a topic.
I think they are progressing very well on several developments. Possibly I'll share more info on request.

Offline john smith 19

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Re: Dawn Aerospace
« Reply #7 on: 08/20/2022 03:14 pm »
Finally some other NSF member got aware of Dawn Aerospace and started a topic.
I think they are progressing very well on several developments. Possibly I'll share more info on request.
Information is always appreciated.

However whenever I see one of these my first question is "So how you handling the Centre-of-Pressure/Centre-of-Mass shifting that's going on as you go from M0 to Mupper-stage-seperation" ?

Hint. Nothing has the operating Mach range of a launcher spaceplane. 

They don't look much different that Radian. I'm not seeing anything very substantial here either.  :(

MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Re: Dawn Aerospace
« Reply #8 on: 08/21/2022 02:13 am »
They don't look much different that Radian. I'm not seeing anything very substantial here either.  :(

???
Radian has no hardware, while Dawn has small scale prototypes. Radian is trying to build a crewed vehicle, while Dawn's goal is an uncrewed smallsat launcher. Radian wants to build an SSTO, and Dawn is only trying for a two-stage design. They aren't really comparable at all.
Wait, ∆V? This site will accept the ∆ symbol? How many times have I written out the word "delta" for no reason?

Offline john smith 19

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Re: Dawn Aerospace
« Reply #9 on: 08/21/2022 10:51 am »

???
Radian has no hardware, while Dawn has small scale prototypes. Radian is trying to build a crewed vehicle, while Dawn's goal is an uncrewed smallsat launcher. Radian wants to build an SSTO, and Dawn is only trying for a two-stage design. They aren't really comparable at all.
I'll admit that was a little harsh. They have complete flight hardware
Radian has been conducting test firings at Brereton airport for some time, but that's about all.

I'm just very weary of a company that shows videos with no humans in shot (for scale) and a flight time of less than 2 minutes.  :( There website says it's 4.8m long (IE just shy of 16 feet) and HTP/Kero. With an empty weight of 75Kg and GTOW of 280Kg thats a structural fraction of 26.7% and a stated goal of M3 to give microgravity of 180secs at above 100Km IE space.

That potentially opens up the market for academic institutions and businesses that want sounding rocket type access with on-demand availablility.  If they sell this as a turn-key package that will be a paradign shift in the industry from solid fuel expendable sounding rockets.

Beyond that  the Cp/Cm shift over the Mach range will be tough with an engine in the tail.

The Mark III is supposed to be 18000Kg and a 250Kg to LEO. That's a payload fraction of 1.38%. Not what you'd expect from a TSTO with an expendable US.  This suggests either
a) It'll be a TSTO and the US will be 1)Cost optimised IE Heavy, expendable or 2)Recoverable and reusable.
or
b) They are going to extend the Mark II into a full SSTO.

a) suggests the funders will take the payload hit, having been convinced the market is there to support it at the price Dawn say they can offer. 2) would be very clever, very bold and very implausible.
b) They are esssentially in Radian territory. Needing either a radical improvement in materials or structural architecture to cut the structural fraction a lot, or some super-duper engine tech to seriously raise the Isp (from 100s to 1000s of seconds).

As with Radian time will tell if they really have something special or if they are playing the Silicon Valley strategy of "Do the easy(ish) bits first and hope/pray some highly-caffinated-engineer/glory hungry intern has an astonishing-deep-insights-giving-a-viable-but-unexpected-solution/one-night-stand with Tony Stark/something- else" happens which solves the problem.

Their plan, as sketched out so far, does not appear capable of delivering the stated end result. The numbers just don't work out.  :( Exactly like Radian.

I will admit the scenery around the airport is pretty spectacular. Something about it said "Colorado" to me :)

More than 3 decades since REL laid out in Spaceflight why Skylon had the engine positions it did and what happens if you try to operate with rear-mounted engines over a large Mach range and it seems that yet another spaceplane startup is going to ignore them.  :(

I will wish them luck and look forward to seeing what progress they make.
« Last Edit: 08/21/2022 10:59 am by john smith 19 »
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Offline TrevorMonty

Re: Dawn Aerospace
« Reply #10 on: 08/21/2022 11:13 am »



???
Radian has no hardware, while Dawn has small scale prototypes. Radian is trying to build a crewed vehicle, while Dawn's goal is an uncrewed smallsat launcher. Radian wants to build an SSTO, and Dawn is only trying for a two-stage design. They aren't really comparable at all.
I'll admit that was a little harsh. They have complete flight hardware
Radian has been conducting test firings at Brereton airport for some time, but that's about all.

I'm just very weary of a company that shows videos with no humans in shot (for scale) and a flight time of less than 2 minutes.  :( There website says it's 4.8m long (IE just shy of 16 feet) and HTP/Kero. With an empty weight of 75Kg and GTOW of 280Kg thats a structural fraction of 26.7% and a stated goal of M3 to give microgravity of 180secs at above 100Km IE space.

That potentially opens up the market for academic institutions and businesses that want sounding rocket type access with on-demand availablility.  If they sell this as a turn-key package that will be a paradign shift in the industry from solid fuel expendable sounding rockets.

Beyond that  the Cp/Cm shift over the Mach range will be tough with an engine in the tail.

The Mark III is supposed to be 18000Kg and a 250Kg to LEO. That's a payload fraction of 1.38%. Not what you'd expect from a TSTO with an expendable US.  This suggests either
a) It'll be a TSTO and the US will be 1)Cost optimised IE Heavy, expendable or 2)Recoverable and reusable.
or
b) They are going to extend the Mark II into a full SSTO.



MK2 is suborbital only vehicle.

MK3 will be expendable 2nd stage with HTOHL booster ie rocket spaceplane. Mass fractions are about right for this RLV, given boosters extra dry mass due to wings and need to RTLS.

Electron is 2.3% as ELV.

Video is first rocket powered flight of MK2 which is quite an achievement especially as its an automous rocket plane built on shoestring budget. Over next few months they should slowly increase altitude.


Offline john smith 19

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Re: Dawn Aerospace
« Reply #11 on: 08/21/2022 02:00 pm »

MK2 is suborbital only vehicle.
Saw that on their website.
Quote from: TrevorMonty
MK3 will be expendable 2nd stage with HTOHL booster ie rocket spaceplane. Mass fractions are about right for this RLV, given boosters extra dry mass due to wings and need to RTLS.
It will be noted that Musk is claiming a 2% payload fraction for Starship, with full reusability.
Quote from: TrevorMonty
Electron is 2.3% as ELV.
Which may be a fairer comparison. The question of course will be how big a payload hit will RL take for booster recovery? If <0.9% they still come out ahead.
Quote from: TrevorMonty
Video is first rocket powered flight of MK2 which is quite an achievement especially as its an automous rocket plane built on shoestring budget. Over next few months they should slowly increase altitude.
[/i]
Let's hope so.
That's sort of the point. Electron can do 2.3% of take off mass.
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Re: Dawn Aerospace
« Reply #12 on: 08/22/2022 04:29 am »
Radian has been conducting test firings at Brereton airport for some time, but that's about all.

I didn't know that. Awesome

More than 3 decades since REL laid out in Spaceflight why Skylon had the engine positions it did and what happens if you try to operate with rear-mounted engines over a large Mach range and it seems that yet another spaceplane startup is going to ignore them.  :(

The website says that the Mk-II's max speed is "Mach 3+". That's SR-71 territory. Difficult, but plenty achievable, particularly when using a rocket rather than an advanced jet engine. A rear engine will be just fine for the Mk-II.

Mk-III is trickier, since first stage typically go much faster (Mach 10 for F9, Mach 16 for Atlas V). I guess it's possible that they intend for the Mk-III to be more of a pop-up rocket, like the crazy and inefficient proposals that have been discussed for making New Shepard a smallsat launcher. In the end I'm not too worried about it, because the Mk-III isn't what they're working on right now. Perhaps when they start actually working on it, they will discover that they have to redesign it to have centrally mounted engines, but that is a problem for later.
Wait, ∆V? This site will accept the ∆ symbol? How many times have I written out the word "delta" for no reason?

Offline john smith 19

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Re: Dawn Aerospace
« Reply #13 on: 08/22/2022 12:39 pm »
I didn't know that. Awesome
Yes. They are not entirely powerpoint engineering.
Quote from: JEF_300
The website says that the Mk-II's max speed is "Mach 3+". That's SR-71 territory. Difficult, but plenty achievable, particularly when using a rocket rather than an advanced jet engine. A rear engine will be just fine for the Mk-II.

Mk-III is trickier, since first stage typically go much faster (Mach 10 for F9, Mach 16 for Atlas V). I guess it's possible that they intend for the Mk-III to be more of a pop-up rocket, like the crazy and inefficient proposals that have been discussed for making New Shepard a smallsat launcher. In the end I'm not too worried about it, because the Mk-III isn't what they're working on right now. Perhaps when they start actually working on it, they will discover that they have to redesign it to have centrally mounted engines, but that is a problem for later.
Yes that's pretty much what I expect them to do.  It puts them back at square one in design terms however.  :( What Mark II teaches them about the flying characteristics of the vehicle is unlikely to transfer to their new Mark III design

I'm not sure what it's made of. If it's CFRC then without serious TPS their operating limits will not be far above M3 anyway.
« Last Edit: 08/22/2022 12:40 pm by john smith 19 »
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Offline TrevorMonty

Re: Dawn Aerospace
« Reply #14 on: 08/22/2022 01:27 pm »
I didn't know that. Awesome
Yes. They are not entirely powerpoint engineering.
Quote from: JEF_300
The website says that the Mk-II's max speed is "Mach 3+". That's SR-71 territory. Difficult, but plenty achievable, particularly when using a rocket rather than an advanced jet engine. A rear engine will be just fine for the Mk-II.

Mk-III is trickier, since first stage typically go much faster (Mach 10 for F9, Mach 16 for Atlas V). I guess it's possible that they intend for the Mk-III to be more of a pop-up rocket, like the crazy and inefficient proposals that have been discussed for making New Shepard a smallsat launcher. In the end I'm not too worried about it, because the Mk-III isn't what they're working on right now. Perhaps when they start actually working on it, they will discover that they have to redesign it to have centrally mounted engines, but that is a problem for later.
Yes that's pretty much what I expect them to do.  It puts them back at square one in design terms however.  :( What Mark II teaches them about the flying characteristics of the vehicle is unlikely to transfer to their new Mark III design

I'm not sure what it's made of. If it's CFRC then without serious TPS their operating limits will not be far above M3 anyway.
The heat loads for suborbital plane shouldn't be that high, see Virgin SpaceShip2.

Offline john smith 19

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Re: Dawn Aerospace
« Reply #15 on: 08/22/2022 05:36 pm »
The heat loads for suborbital plane shouldn't be that high, see Virgin SpaceShip2.
Except Mark III is not designed to be a sub-orbital plane.

It's designed as the booster stage for a full up orbital launch vehicle.

Staying with a maximum speed of M3 leaves the upper stage needing to make 19-20Machs to get to orbit.

Historically the rule of thumb has been to split the delta 50/50 booster to US, but F9 its more 1/4-3/4s, so at least M6.

So I think it's safe to say Mark III will need to at least double the top speed of Mark II.

Time will tell how that works out for them.
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Offline CameronD

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Re: Dawn Aerospace
« Reply #16 on: 08/22/2022 11:36 pm »
James Powell on LinkedIn:
Quote
Pushing toward 40 flights, averaging just under 1 a week now.
With sufficient thrust, pigs fly just fine - however, this is not necessarily a good idea. It is hard to be sure where they are
going to land, and it could be dangerous sitting under them as they fly overhead.

Offline FutureSpaceTourist

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Re: Dawn Aerospace
« Reply #17 on: 09/21/2022 10:39 am »

Offline john smith 19

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Re: Dawn Aerospace
« Reply #18 on: 09/21/2022 01:02 pm »

OMG I knew it was small but it's actually tiny

It's teeny tiny.  :)

That moment at the end surrounding the vehicle was a real LOL moment.  :)

I thought it was an airport, but actually, I think it's a road.

This has put a real smile on my face. Both very serious and utterly hilarious at the same time.

That said GNC and flight dynamics issues dont really scale (except when they get worse), so there's a lot to be said to solving issues with them at the smallest possible scale, before you scale up, so the control systems are rock solid. If they couldn't get it flying well at this scale they'd be doomed when they scale up.

I'll wish them well with their test plan.
« Last Edit: 09/21/2022 01:07 pm by john smith 19 »
MCT ITS BFR SS. The worlds first Methane fueled FFSC engined CFRP SS structure A380 sized aerospaceplane tail sitter capable of Earth & Mars atmospheric flight.First flight to Mars by end of 2022 2027?. T&C apply. Trust nothing. Run your own #s "Extraordinary claims require extraordinary proof" R. Simberg."Competitve" means cheaper ¬cheap SCramjet proposed 1956. First +ve thrust 2004. US R&D spend to date > $10Bn. #deployed designs. Zero.

Offline TrevorMonty

Re: Dawn Aerospace
« Reply #19 on: 09/21/2022 05:52 pm »

OMG I knew it was small but it's actually tiny

It's teeny tiny.  :)

That moment at the end surrounding the vehicle was a real LOL moment.  :)

I thought it was an airport, but actually, I think it's a road.

This has put a real smile on my face. Both very serious and utterly hilarious at the same time.

That said GNC and flight dynamics issues dont really scale (except when they get worse), so there's a lot to be said to solving issues with them at the smallest possible scale, before you scale up, so the control systems are rock solid. If they couldn't get it flying well at this scale they'd be doomed when they scale up.

I'll wish them well with their test plan.
They operate out of strip near Mt Cook. COVID would of reduced tourist scenic flight air traffic considerably as borders have been closed for two years.

 

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