Category Archives: Space

A Couple Other Armadillo Notes

I missed this part of John Carmack’s talk somehow, but it would seem to be news that Jeff Foust picked up on:

At the 2008 Lunar Lander Challenge last October, Rocket Racing and Armadillo Aerospace announced a joint venture to develop vertical takeoff, vertical landing vehicles for suborbital space tourism. However, Armadillo Aerospace founder John Carmark revealed at Space Access ‘09 this morning that this deal—at least, as announced in October—has fallen through. Carmack said that while there are relationships with both Rocket Racing and an unnamed third party, the deal as announced “did not come to fruition”. Carmack added, though, that he anticipates making some announcements in the next month that may be related to any suborbital vehicle work.

If so, he’s not the first to have run into issues working with Granger Whitelaw. Likely he’ll not be the last, either.

And I didn’t mention it in my previous post, but this was news as well, I think:

Will be competing for Level Two this year, and they hope to make their attempts from their home field when season begins in July.

My emphasis. I hadn’t heard this before. I think that it may be the first public announcement of the beginning of the competition season. I wonder if John was supposed to make it?

Jim Muncy

In about half an hour, Jim Muncy of the Space Frontier Foundation will be talking about space policy issues, particularly the dreaded Gap. Look for live updates after the current break, when I get back to the computer.

[OK, speech starting]

Jim (unusually) has charts. Title: Mind The (Space) Gap. Another troublemaking project of the Space Frontier Foundation.

Back in 2005 CEV (Orion) was not aimed at ISS. No requirement for ISS, and Steidle didn’t want it to. Number of innovative architectures considered. Steidle proposed a “nontraditional crew” development effort over 2005-2008 to address if you could take the Burt Rutan SS1 approach and use the commercial market to build the reliability of human earth/orbit systems so that NASA wouldn’t have to “human rate” vehicle that would launch CEV. CEV could go up uncrewed, and meet crew on orbit. At that time, NASA forecast a four-year gap from 2010 to 2014, even with risk reduction of two CEV contractors and nontraditional effort. That was the plan.

Then came Mike. Had to get rid of the gap. Was “unseemly in the extreme” for the US (read NASA) to not have a human launch capability, maybe even a national security issue. It was no longer about getting NASA beyond earth orbit, but it became about “closing the gap” because it was just wrong for NASA not to launch humans into space. He says that it’s not Apollo on steroids, it’s Gemini on steroids. What we’d be left with after Ares 1 and Orion would be Gemini in capability, with a larger capsule.

Some doubted hysteria, and didn’t think we could afford to both close gap and achieve VSE goals, and that it wasn’t a national security threat to not be able to launch astronauts into space on NASA vehicles. But some Senators insisted (with zero evidence) that it was.

So we lost the goal of the vision, of affordable and sustainable. The brightest guys in the room, the rocket scientists, decided to pull a bait and switch. They decided to use the ISS as an excuse for developing the new vehicle to close the gap, even though they defunded the research at the station to pay for their new rocket. They thought that this was the one and only opportunity to develop a new launch vehicle. It wasn’t really designed to close the gap, it was designed to go to Mars. But that’s not how it was sold, and they rammed through a transportation system as though it was the B-52, something to be used for over half a century to do everything NASA would be doing. And the story was that it was a Shuttle-derived approach that would close the gap down to 2012. It would be Safe, Simple and Soon.

How is that working out? NASA’s current forecast is calendar year 2017. $44B to Initial Operating Capability, so gap has grown by three years from original VSE goal. Slipped five years from ESAS goals of three and a half years ago, or 1.3 years per year (new NASA metric YPYS — Year per year slip). So much for new exploration.

No way NASA gets to the moon by 2019 if it only launches Ares 1 in 2017. May not get there until 2029 (Apollo sixtieth anniversary), if ever, and it won’t be “affordable” or “sustainable” or fit under likely budget. “We are spending a lot of money in DC right now.” Do you see politicians throwing a lot of money at NASA? No. NASA is not seen as stimulating the economy, or developing technology, or relevant. Some of have noted and said this for years. Doesn’t fit the budgets as they’re likely to be, and NASA never gets back to exploring. Betrayal of a third presidential mandate in space (first was space station, second was Bush 39 SEI, also known as staff expansion initiative, and now VSE). Presidents have set goals for space, but the agency hasn’t been honoring them. And even leaving aside exploration, NASA has failed by its own metric of clsoing the gap. You don’t have to argue about the technical details, or even that it’s going to be too expensive to operate. All you have to do is point out that with this plan the gap has increased from four years to six or seven years. In the administrator’s words, this architecture is unseemly, a national security threat, disinspiring our youth.

We are now in the era of hope and change. We can fix mistakes with a new administration and congress. The fastest safest/cheapest/approach is to utilize existing/developing commercial ELVs to launch simple human-carrying spacecraft (i.e., COTS D).

SFF thinks it’s time to declare Ares 1 and ESAS a failure. NASA should use its stimulus funds to stimulate a new human ETO industry by funding multiple COTS D concepts. Launch Orion on EELV. Pursue “cheapest” medium-heavy option for exploration and intermodal demos.

When NASA claims that Ares 1 is needed for Orion they’re fudging the numbers, because the abort system for Ares 1 is heavier than it would be for an EELV, because the former cannot be shut down and the abort system has to outrun it.

Has no problem with Shuttle Z or some other cheap and dirty approach to launching fifty or sixty metric tons at a time, but have to do something so that fifty years after we landed a man on the moon we can land a man on the moon. It’s easy to fix the problem if we only mind Mike Griffin’s first suggestion, and actually mind the space gap.

In response to a question, he still professes optimism about the administration. There is someone at OSTP (Mike Kleegle ) who wants to build partnerships with private industry, and he hopes that there will be an administrator and deputy who will implement it. He was hoping for Isakowitz, but his appointment was killed by Senator Nelson. His comment about Senator Nelson’s cerebral propensity was off the record, so I won’t repeat it.

Masten Space Systems

Dave Masten: small company developing VTVL vehicles, like Armadillo. Based in Mojave with small team. Have been working on the last year developing reliable igniter (they’ve sold one) and a 500 lbf-thrust engine. Since last year they lost teh XA-0.1 vehicle on a tether, breaking off landing gear when it swung, and then breaking off the tether, landing on the engines. Vehicle relatively intact, but went on to new vehicle, XA-0.1B that used the old engines. Moving to new lower-maintenance, second-generation engine now, with 750 lb-f thrust. Did sixty tests of engine with six injector sets, and ended up with 120-second firing, which was depletion of test-stand propellant.

XA-0.2 still being built, and expect to fly it by the end of the year.

Michael Mealling describing business over the past year. Getting interest in people on new 750 lbf engine. Responding to various RFIs for low-altitude and high-altitude spaceflight. Encouraged by Ames suborbital reusable payload program.

Ben Brockert now briefing more engine details. Target Isp of 220 seconds. Has lower chamber pressure than earlier engine. Cooper now, aluminum later for chamber. Durable, can run to both fuel or oxidizer exinction. Pintle injector, with independent fuel and oxidizer injectors. Three of each, allowing nine combinations, as well as different fuel densities. Want test trailer to be as close as possible to operating vehicle, so brains for trailer same as those for vehicle. Target date for flying the single-engine vehicle is this month (April). Announcing it here, if they don’t make it, feel free to make fun of him at Arocket. Happy engine died because he was getting tired of fixing old engines.