Author Topic: Stratolaunch: General Company and Development Updates and Discussions  (Read 1052208 times)

Online yg1968

  • Senior Member
  • *****
  • Posts: 17529
  • Liked: 7266
  • Likes Given: 3114

Offline Lars-J

  • Senior Member
  • *****
  • Posts: 6809
  • California
  • Liked: 8487
  • Likes Given: 5385
Update on Stratolaunch:
http://spacenews.com/stratolaunch-considering-using-multiple-launch-vehicles/

From the article:
Quote
That near-term focus on alternative launch options means Stratolaunch is deferring work on a crewed vehicle that would launch on the Orbital ATK booster. At the International Astronautic Congress in Toronto in October, Stratolaunch and Sierra Nevada Corp. announced they were studying the development of a 75-percent-scale version of Sierra Nevada’s Dream Chaser spacecraft.

“What we’ve decided to do is kind of take a pause on further development of that,” he said, as Stratolaunch examines alternative launch options.

Not a ringing endorsement of OrbitalATK & SnC. (or perhaps their own business model, if they are deferring development)

Online yg1968

  • Senior Member
  • *****
  • Posts: 17529
  • Liked: 7266
  • Likes Given: 3114
Looks like Paul Allen has announced a new arm of his investment fund to develop various concepts which the Stratolaunch system will support, and it's called.......Vulcan Aerospace.  ::)

(no this is not a co-incidence as Allen is trying stop ULA from using that name, although since I thought Vulcan Inc. is an investment fund the protest will probably come to nothing)

The most interesting part of that press release is this part:

Quote
The Stratolaunch aircraft is about 80% fabricated and 40% assembled, and is on track for first flight in 2016.

Online yg1968

  • Senior Member
  • *****
  • Posts: 17529
  • Liked: 7266
  • Likes Given: 3114
Update on Stratolaunch:
http://spacenews.com/stratolaunch-considering-using-multiple-launch-vehicles/

From the article:
Quote
That near-term focus on alternative launch options means Stratolaunch is deferring work on a crewed vehicle that would launch on the Orbital ATK booster. At the International Astronautic Congress in Toronto in October, Stratolaunch and Sierra Nevada Corp. announced they were studying the development of a 75-percent-scale version of Sierra Nevada’s Dream Chaser spacecraft.

“What we’ve decided to do is kind of take a pause on further development of that,” he said, as Stratolaunch examines alternative launch options.

Not a ringing endorsement of OrbitalATK & SnC. (or perhaps their own business model, if they are deferring development)

More Orbital ATK than DC, it would seem. The article seems to imply that it would take too long to build the Orbital LV and that it would also be expensive.

Quote
A smaller vehicle, he said, could be developed more quickly and less expensively. “It takes a more near-term focus on revenue generation,” he said.
« Last Edit: 04/16/2015 01:11 am by yg1968 »

Offline Archibald

  • Senior Member
  • *****
  • Posts: 2611
  • Liked: 500
  • Likes Given: 1096
I wonder how much payload could be orbited by a J-2X S-IVB stage (pretty much an expendable SSTO) air-launched by a Roc...
Han shot first and Gwynne Shotwell !

Offline R7

  • Propulsophile
  • Senior Member
  • *****
  • Posts: 2725
    • Don't worry.. we can still be fans of OSC and SNC
  • Liked: 992
  • Likes Given: 668
Update on Stratolaunch:
http://spacenews.com/stratolaunch-considering-using-multiple-launch-vehicles/

Quote
Orbital ATK is developing the rocket, which uses solid-fuel lower stages and an upper stage powered by RL-10 engines from Aerojet Rocketdyne.

Didn't liquid upper stage get the axe ??

The most interesting part of that press release is this part:

Quote
The Stratolaunch aircraft is about 80% fabricated and 40% assembled, and is on track for first flight in 2016.

So since January fabrication percentage hasn't increased and almost 40% assembly progressed to 40%.

If Stratolaunch wants smaller boosters will OATK consider it too much of a direct competitor or make Roc drop Tauruses Minotaurs?
« Last Edit: 04/16/2015 06:26 am by R7 »
AD·ASTRA·ASTRORVM·GRATIA

Offline R7

  • Propulsophile
  • Senior Member
  • *****
  • Posts: 2725
    • Don't worry.. we can still be fans of OSC and SNC
  • Liked: 992
  • Likes Given: 668
The creation of Vulcan aerospace and the tidbits we know about it makes me thinking.
How about Stratolaunch to fill an orbital propellant depot ? 13500 pounds isn't that much, then it is all a matter of frequent flights (or not)
Do they plan a second Roc aircraft ?
How often could they fly ? once a week ? once a day ?

Stratolaunch system does not scream cost-competitiveness and for a larger propellant hauling market it would have to be against you-know-who-X.
AD·ASTRA·ASTRORVM·GRATIA

Offline newpylong

  • Full Member
  • ****
  • Posts: 1499
  • Liked: 200
  • Likes Given: 343
I wonder how much payload could be orbited by a J-2X S-IVB stage (pretty much an expendable SSTO) air-launched by a Roc...

Liquid let alone Hydrolox air launch?  huh?

Offline RanulfC

  • Senior Member
  • *****
  • Posts: 4595
  • Heus tu Omnis! Vigilate Hoc!
  • Liked: 900
  • Likes Given: 32
Well, they discussed it in terms of absolute costs, not relative to something on the ground. A dedicated carrier aircraft--i.e. one that cannot do anything else and where all the costs are charged to the launcher program--is apparently a big chunk of the overall operating costs. So getting that cost down is an important way to reduce the overall program costs.

Simply maintaining the certification, license, training and pilots is going to cost money. Think about that L-1011 that Orbital uses--it has three pilots. If it launches only one rocket per year, the salary and training costs of those three pilots have to be charged entirely to that single launch. Now maybe those guys are on retainer and they spend the rest of the year flying 737s for Southwest or something and only show up at Orbital when needed, but Orbital has to pay for their certification and training on the unique L-1011. That cannot be cheap. Same is true for the maintenance guys and everything specific to that aircraft.

Stratolaunch is going to have the same issues.

This was also discussed extensively by AirLaunch and others before:
http://mae.engr.ucdavis.edu/faculty/sarigul/papers/AIAA-2008-7835.pdf
http://mae.engr.ucdavis.edu/faculty/sarigul/aiaa2001-4619.pdf
http://arc.aiaa.org/doi/abs/10.2514/6.2013-5422
etc...

The key-word of course is "dedicated" and as has been proven by Pegasus/L1011 if you ONLY use the carrier for air-launch and you ONLY launch a few times a year your per-flight costs are enormous. This is assumed with StratoLaunch because the announced PURPOSE of the carrier aircraft is for launch but its not fully a given either. To put it perspective any carrier aircraft that can carry an LV can carry a cargo-pod as well and there is in fact a very lucrative and proven market for large cargo carry in the world today. IF (and I will be the first to admit its a big if) this is true then the carrier aircraft can be employed for other purposes at times when it is not scheduled for use as an LV carrier aircraft and many of the suggested issues go away.

I highly suspect that the main reason why StratoLaunch went with a fully custom aircraft was driven by payload-to-orbit and LV sizing but with a secondary purpose in mind as well. Otherwise they COULD have gone with a less expensive and more versatile carrier aircraft such as a converted 747 freighter as suggested by AirLaunch above.
(Compare that the current Pegasus-II is aimed at a gross weight of 465,000lbs where as the AL-LV was a little over 207,000lbs. Pegasus-II is aimed at delivering 13,500lbs to orbit where as the AL-LV had {can't find my references atm} around 10,000lbs IIRC)

It was pointed out in the cited paper that the AL carrier aircraft could still be used as either a freighter or a water-bomber (due to the system installed to balance the AC at launch) as a secondary economic mission after modification to carrier aircraft. With it's more "modular" nature by design it is hard to imagine the StratoLaunch AC would be ONLY capable of the carrier AC mission.

Randy
From The Amazing Catstronaut on the Black Arrow LV:
British physics, old chap. It's undignified to belch flames and effluvia all over the pad, what. A true gentlemen's orbital conveyance lifts itself into the air unostentatiously, with the minimum of spectacle and a modicum of grace. Not like our American cousins' launch vehicles, eh?

Offline RanulfC

  • Senior Member
  • *****
  • Posts: 4595
  • Heus tu Omnis! Vigilate Hoc!
  • Liked: 900
  • Likes Given: 32
Or...

Maybe Paul or someone he knows was involved with this project:
http://deepblue.lib.umich.edu/bitstream/handle/2027.42/77293/AIAA-1993-3955-297.pdf?sequence=1

And just really, really, really wanted to see this thing in action :)
(It's not to late to change the name from Pegasus-II to Gryphon :) )

Randy
From The Amazing Catstronaut on the Black Arrow LV:
British physics, old chap. It's undignified to belch flames and effluvia all over the pad, what. A true gentlemen's orbital conveyance lifts itself into the air unostentatiously, with the minimum of spectacle and a modicum of grace. Not like our American cousins' launch vehicles, eh?

Offline Archibald

  • Senior Member
  • *****
  • Posts: 2611
  • Liked: 500
  • Likes Given: 1096
Quote
http://arc.aiaa.org/doi/abs/10.2514/6.2013-5422

Thank you for that link. I always wondered how much payload to orbit could a 747-400F rocket lift. 747-400F are cheap, they are many, and they can lift 305 000 pounds on their back.
The booster described in the paper has three Merlins and three RL-10s - exactly half of a Saturn I :p, not far from an Atlas-Centaur in fact.
End result ? 47 000 pounds to orbit, a very respectable number. By replacing the 747F with an An-225 and the Merlin with high performance NK-33s, it must be possible to lift much more than 50 000 pounds to orbit, perhaps the shuttle 65000 pounds, who knows.
Han shot first and Gwynne Shotwell !

Offline Patchouli

  • Senior Member
  • *****
  • Posts: 4490
  • Liked: 254
  • Likes Given: 457
I wonder how much payload could be orbited by a J-2X S-IVB stage (pretty much an expendable SSTO) air-launched by a Roc...

A single staged rocket with one SSME launched from the ground can place 10,000lbs in orbit.
http://www.spacefuture.com/archive/a_single_stage_to_orbit_thought_experiment.shtml

If air launched this of course would be somewhat higher maybe 12,000lbs since the rocket would have lower gravity losses and would not have to fight it's way through the denser air at low altitude.
Maybe even more if an altitude optimized nozzle is used.
A J-2X stage would be much lower unless SRBs are used to off set it's lower thrust.

Ironically air starting a SSME on a rocket dropped from an aircraft might be easier then it was on Ares I.
Use something like the harness and parachute used on QuickReach to turn the rocket vertical and the engine may see enough head pressure to start after falling for a few seconds.

A stage with two SSME's or J-2Xs and a small upper stage may get close to Falcon 9 V1.0 performance.
The limiting factor would be the total mass the carrier aircraft can safely take off and the maximum dimensions of the aircraft's payload.

Quote
http://arc.aiaa.org/doi/abs/10.2514/6.2013-5422

Thank you for that link. I always wondered how much payload to orbit could a 747-400F rocket lift. 747-400F are cheap, they are many, and they can lift 305 000 pounds on their back.
The booster described in the paper has three Merlins and three RL-10s - exactly half of a Saturn I :p, not far from an Atlas-Centaur in fact.
End result ? 47 000 pounds to orbit, a very respectable number. By replacing the 747F with an An-225 and the Merlin with high performance NK-33s, it must be possible to lift much more than 50 000 pounds to orbit, perhaps the shuttle 65000 pounds, who knows.

The best engine to use might be the BE-3 with a larger expansion ratio with a RL-10 upper stage.

With kerosene TAN it could even be a near SSTO for payloads such as a close to full sized Dream Chaser.

Keep the large hybrids or have Xcor engines inside DC to act as a second stage/LAS.
It could give Spacex a run for their money in the LEO market.
GTO not so much as unless a cheap RL-10 replacement can be found.

More daring would be put the BE-3s with TAN inside Dream Chaser and run a drop tank like MAKS-OS but this would mean trusting the stack to not do any RUDs for crewed missions.

« Last Edit: 04/20/2015 05:30 am by Patchouli »

Offline RanulfC

  • Senior Member
  • *****
  • Posts: 4595
  • Heus tu Omnis! Vigilate Hoc!
  • Liked: 900
  • Likes Given: 32
The cited paper is here:
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20140003206.pdf

And it's NOT a very good design or launch method. It assumes top-mounted and airfoils are required which greatly degrades the LV performance from the start. "Sizing" it for maximum diameter... Well the paper goes on to show that anything done outside the last DARPA "air-launch" study (which for no specified reason rejects any concept BUT top-mounted, airfoil equipped LVs) is ignored.

Frankly even mentioning StratoLaunch and SS-2 in the report seems an attempt to draw attention away from those designs rather than including them.

Randy
From The Amazing Catstronaut on the Black Arrow LV:
British physics, old chap. It's undignified to belch flames and effluvia all over the pad, what. A true gentlemen's orbital conveyance lifts itself into the air unostentatiously, with the minimum of spectacle and a modicum of grace. Not like our American cousins' launch vehicles, eh?

Offline Katana

  • Full Member
  • ***
  • Posts: 378
  • Liked: 49
  • Likes Given: 20
Quote
http://arc.aiaa.org/doi/abs/10.2514/6.2013-5422

Thank you for that link. I always wondered how much payload to orbit could a 747-400F rocket lift. 747-400F are cheap, they are many, and they can lift 305 000 pounds on their back.

How to release the rocket from back?
You know what happens to SR71/D-21...

Offline Patchouli

  • Senior Member
  • *****
  • Posts: 4490
  • Liked: 254
  • Likes Given: 457

How to release the rocket from back?
You know what happens to SR71/D-21...
They were able to release the Shuttle from the back of the 747 without any mishaps during the ALT tests.
Though the ALT test shuttle was about 200,000lbs about a 100,000lbs lighter then the booster.
Separation dynamics are a lot easier at subsonic speeds then they are at mach 3.
The Stratolaucher design is supposed to be much safer then carrying the payload in the dorsal position.
« Last Edit: 04/25/2015 08:01 pm by Patchouli »

Offline Katana

  • Full Member
  • ***
  • Posts: 378
  • Liked: 49
  • Likes Given: 20

How to release the rocket from back?
You know what happens to SR71/D-21...
They were able to release the Shuttle from the back of the 747 without any mishaps during the ALT tests.
Though the ALT test shuttle was about 200,000lbs about a 100,000lbs lighter then the booster.
Separation dynamics are a lot easier at subsonic speeds then they are at mach 3.
The Stratolaucher design is supposed to be much safer then carrying the payload in the dorsal position.

So the rocket need a wing bigger than shuttle to have similiar aerodynamics.

Gliding like shuttle with full fuel...

Offline RanulfC

  • Senior Member
  • *****
  • Posts: 4595
  • Heus tu Omnis! Vigilate Hoc!
  • Liked: 900
  • Likes Given: 32
Quote
http://arc.aiaa.org/doi/abs/10.2514/6.2013-5422

Thank you for that link. I always wondered how much payload to orbit could a 747-400F rocket lift. 747-400F are cheap, they are many, and they can lift 305 000 pounds on their back.

No they can carry that much payload INSIDE, with modifications they can carry SOME loading on their back but the more is 'outside' the normal framing the more modification needed.

Even the ALT 747 needed mods (as did the Orbiter carrier aircraft, and note the DARPA/NASA report specifies using THOSE aircraft not "regular" 747s) and that's still a bit short of "full" loading. To carry the suggested LVs would require (and the report notes this) even more modifications.
(And the AirLaunch modified 747 cost about 20 million IIRC)

Quote
The booster described in the paper has three Merlins and three RL-10s - exactly half of a Saturn I :p, not far from an Atlas-Centaur in fact.
End result ? 47 000 pounds to orbit, a very respectable number. By replacing the 747F with an An-225 and the Merlin with high performance NK-33s, it must be possible to lift much more than 50 000 pounds to orbit, perhaps the shuttle 65000 pounds, who knows.

Saturn-1 (H1's to be specific) were a bit less than 1.5 times more thrust than the Merlin-1D :) But being even more specific this is NOT something that StratoLaunch seem interested in. They seem "happy" with the rather crappy performance of an all solid launcher. Given how much mass would be required to get a liquid launcher to "play" as well with a doing its own gamma maneuver I can probably see their point :)

So the rocket need a wing bigger than shuttle to have similiar aerodynamics.

Gliding like shuttle with full fuel...

Pretty much which is why "I" for one don't buy the DARPA/NASA report :) I suspect there's an "assumption" of some sort on having some separation rockets attached but they are not mentioned in any of the reports.

Bottom carry/drop has a LOT fewer issues all around but any LV that has to perform its' own Gamma maneuver is going to have to be pretty solid (pun intended :) ) -ly built. The StratoLaunch Pegasus-II has to do the same thing but its dropping away from the carrier at the same time its lighting up the engine.

Randy
From The Amazing Catstronaut on the Black Arrow LV:
British physics, old chap. It's undignified to belch flames and effluvia all over the pad, what. A true gentlemen's orbital conveyance lifts itself into the air unostentatiously, with the minimum of spectacle and a modicum of grace. Not like our American cousins' launch vehicles, eh?

Offline arachnitect

  • Member
  • Full Member
  • ****
  • Posts: 1553
  • Liked: 501
  • Likes Given: 759
http://www.seattletimes.com/business/boeing-aerospace/space-wa2/

Quote
But now that human spaceflight plan is shelved, along with Orbital’s planned rocket.

[Vulcan Aerospace president Chuck Beames] said Orbital’s rocket “was not hitting the economic sweet spot to generate revenue,” so Vulcan has reopened the design plan and is “evaluating over 70 different launch vehicle variants.”

Offline FutureSpaceTourist

  • Global Moderator
  • Senior Member
  • *****
  • Posts: 50668
  • UK
    • Plan 28
  • Liked: 85176
  • Likes Given: 38157
Oh dear, I fear all 70 variants may come back with the same answer - air launch isn't economic, especially given both the cost of developing the huge aircraft & new/modified rocket and the increasing innovation - leading to cost reductions - in other parts of the market (SpaceX, Blue Origin, ULA's Vulcan rocket, potential small-sat launchers etc).
« Last Edit: 06/01/2015 12:12 pm by FutureSpaceTourist »

Online Robotbeat

  • Senior Member
  • *****
  • Posts: 39358
  • Minnesota
  • Liked: 25386
  • Likes Given: 12163
It can be economic, but you can't jut hobble together a rocket for it.

I heard about this at a conference. They will complete the aircraft in spite of the launch vehicle being shelved.
Chris  Whoever loves correction loves knowledge, but he who hates reproof is stupid.

To the maximum extent practicable, the Federal Government shall plan missions to accommodate the space transportation services capabilities of United States commercial providers. US law http://goo.gl/YZYNt0

 

Advertisement NovaTech
Advertisement Northrop Grumman
Advertisement
Advertisement Margaritaville Beach Resort South Padre Island
Advertisement Brady Kenniston
Advertisement NextSpaceflight
Advertisement Nathan Barker Photography
1