Follow the Build: Q&A with XCOR CEO Jeff Greason

Yesterday we interviewed XCOR Chief Executive Officer Jeff Greason (@JeffGreason on Twitter) about Lynx status, the future of suborbital and orbital space flights, and fielded questions from Facebook and Twitter.

Thanks to all of you who submitted questions–both for your thoughts and your patience. Enjoy!

Bryan Campen: If we were to step into the hangar right now, what would we see?

Jeff Greason: So what you would see are a few things. You’d see that the hydrogen stand we are doing engine work on with ULA is very prominent.

And the propulsion test bed that we are doing Lynx development on is out in the hangar as well.

Then, off behind a black curtain, we are accumulating the composite pieces of the Lynx airframe. We have:

• The fuselage we are going to fly,
• The LOX tank we are going to fly is currently being installed in the fuselage,
• We have the strakes—the thick part at the base of the wings–on both the port and starboard side,
• We have the landing gear,
• And we are eagerly awaiting the cockpit. It’s one of those things that is very close, but hard to tell how long it takes to get all the way to done.

BC: What major milestones are shaping-up this year for XCOR and Lynx? 

JG: When we get all the pieces for Lynx, of course that’s gonna be a big day.

There are a few pieces we need to start with the final assembly of the vehicle: the strakes, fuselage and cockpit.

Once we have those we’ll start integrating and doing all of the vehicle structural assembly. After all of that is done it starts to look like a spaceship. Then we start wiring and plumbing it. And there are other pieces that bolt on rather than glue on, like the engine cowling, that will arrive during the Lynx wiring and plumbing process.

Parallel to all this we continue to shake the kinks out of the propulsion system.

When the propulsion system is ready to go, we unbolt it from the test stand and bolt it on to the bird.

And when the bird is ready to go we start flight test activity.

BC: Jos Gal asks: When will be the roll-out of the Lynx and when is the first test-flight?

JG: I believe we will see the flight test program starting this year.

The roll-out will of course be when the vehicle is put together and the first flight test will be when it is ready to fly.

We’re in the phase of the project where we have to knock the remaining issues down one by one. Our engineers are going as fast as they can to get there, so there’s no need to apply pressure with a flight date.

BC: Per Wimmer asks: What are the most important milestones between now and launch of XCOR Lynx Mark I? How is everything progressing?

JG: To go back to the earlier answer—the next major milestone is when we have all of the structural subassemblies to start the vehicle assembly.

And it’s hard to pick out one major milestone after that. It’s the process of getting all the pieces put together.

There will be another, separate path when we are done debugging the propulsion system, at least sufficiently for the Mark I flights to start.  But those are not dependent on each other, because we have the testing on the test stand while we have the vehicle integration happening in parallel.

Those are the major milestones between here and flight.

As to how it’s progressing, I am optimistic and feeling good about the process once we have all the pieces in place. It’s a little hard to predict when we will have all the pieces.

BC: Follow-up question from Per Wimmer: How do you see the competitive landscape for private space rocket building and space travel developing at the moment?

JG: Right now, and for the next several years, the suborbital and orbital markets are going to remain fairly distinct from each other. They are not overlapping segments.

In the suborbital arena more than one company is going to enter service, and we’ll be one of them. I’m feeling very comfortable with our ability to compete on price because of our lower capital costs and higher flight rate, with the other entrants that I see coming into the suborbital market.

For the next few years, the orbital market is going to remain dominated by expendable launch vehicles, and I support efforts to reuse. But that will take some time to come online and reuse will likely work very incrementally in the near- to mid-term. I don’t think that there is going to be a day when suddenly it’s all reusable, with very low maintenance labor. I think it’s going to be a long, evolutionary process.

In the orbital world for the next few years, I think the story is going to be SpaceX, ULA and Orbital Sciences competing for market share. And of course ULA is a customer of ours trying to develop cheaper engines to help them compete, and we fully support them!

The generation after Lynx, on the one hand, will be starting immediately after Lynx Mark I; we will start the Lynx Mark II build.

But we also have, as we’ve said many times, a fully reusable orbital system on the drawing board. Just how fast we are going to start on that remains to be seen. But certainly it’s a multi year effort to get that to a point where it’s ready to start flight-testing.

I think eventually at much higher flight rate, reusable orbital systems will come into the market place. And when that happens they will dominate the lower end of the market.

That said, I think that expendable or quasi-reusable launch vehicles are going to remain. Because I think the market will optimize where the bulk of the mass gets lifted in smaller packages on vehicles that fly very frequently, but are small. And at the same time, the few pieces that are inconvenient to break into small payloads will be an oversized payload market, and that will continue to be served by expendables and semi-reusables.

BC: @ssshocker on Twitter asks: What is the timeline for Lynx MKIII? What price point are you aiming for with LEO payloads?

JG: I am not going to speculate on the timeline for Mark III. After the Mark I is flying I’ll put a new number on it.

Right now it’s looking like that will be about $500,000 for a microsatellite launch. The price is dominated by the cost of the expended upper stage for Mark III.

BC: Hernan Estrada asks: How do you expect XCOR technology (and its competitors’) to impact commercial point-to-point flying 10 years from now?

JG: I know there is an enormous level of interest in high speed point-to-point transport. And I believe that the day will come when these kinds of technologies do play in that market.

But I don’t expect it to be a material factor within ten years. The reason for that is that point-to-point transport, unlike suborbital and orbital flight, directly competes with a very mature industry of subsonic aircraft.

For the commodity you are offering—high speed—that’s a small fraction of the market who want that speed so badly that they will get themselves to a space port in a remotely populated area in order to take a high speed flight.

So in order for high speed flight to be practical, you have to be able to do it, and you have to be able to do it at a price point that is reasonably competitive with subsonic aircraft, or at least not a large multiple of it. On top of that, you would need to be able to fly from densely populated areas with all the implications that has for how you integrate with the air traffic control system, how much noise you generate on takeoff, that kind of thing.

It is possible to do. But I think it’s going to take many generations of a reusable rocket vehicle before we’re ready to do them. And that means I think suborbital point-to-point flight over any significant distance, as a major form of transportation, is going to come on only after we have fully reusable orbital flight.

Now people will find certain high value uses where an orbital system can be turned into a point-to-point delivery system for a few very high value payloads, where nobody cares how much it costs if it gets there in time. But I don’t that is going to be a major factor in the point-to-point transportation market over the next ten years.

Twenty? Maybe.

BC: @silicon_sky on Twitter asks: Is there a plan to try an intercontinental flight with the Lynx?

…and is there a one sentence answer you want to give with that?

JG: I have a more than one sentence answer with that one [laughter]. I get asked this question a lot.

The only way to get long distance out of a rocket is to go very, very fast. And if you want to go a significant fraction of the way around the planet, you have to go a significant fraction of the velocity it takes to go into orbit. Very significant point-to-point distances are just not acceptable to suborbital vehicles of the first generation because while you can go 60 or 70 miles high, you can’t go more than about 200 miles downrange. To extend that you could use subsonic glide, but that’s not any faster than any other airplane.

So it’s only interesting when you’re talking about orbital class systems that go Mach 8, Mach 10 or beyond.

BC:  @Goolic on Twitter asks: I’m really curious if you see any significant difference/advantage vs Virgin or simply see the market as big enough?

JG:  What’s important right now, and what we focus on, is getting multiple successful entrants operating in the suborbital market so that we can start to compete with each other. Once multiple companies are serving that market, they will all try different things and offer different kinds of services to the customers. And really not until then will we find out what the demands of the market really are.

So I don’t spend a lot of time thinking about what the various competitive situations are going to be, or gaming them out.

What I focus on is “Let’s get out there and start serving the market, and then we’ll find out!” Maybe a market segments, and different companies offer different services that appeal to different people. Maybe the market’s big enough for many entrants. Or maybe there are winners and losers, and in that case we will work very hard to be one of the winners.

But until there are multiple companies in the competitive marketplace it’s too early to worry about.

BC: Question from Julian Powell: Any updates on the development of the upper stage hydrolox engine for ULA?

JG: The program is continuing, the work is ongoing, and when we reach significant milestones we ask permission to say something public about them. And ULA has been great about that.

BC:  @ZacTrolley asks: International partners & employees; how difficult is it [with] ITAR and other security measures? How can it be made easier?

JG: With ITAR in place it is essentially not possible for us to have non-US persons as employees. All of our employees are citizens or US permanent residents.

There is ITAR reform underway in the United States, and I think it’s possible in time those restrictions will come down, but they are not down yet and might not be down soon.

BC: @tschwarzzz on Twitter asks: What is your long-term vision for XCOR, as far as space settlement goes? Do you envision a future Lynx that enables it?

JG: So I outlined earlier that there is a plan for a fully reusable orbital system after Lynx. And I also discussed that, in my own view, the orbital transportation system is going to shake down into small, highly reusable vehicles that fly most of the mass, and larger semi-expendable vehicles that fly far less frequently that carry the occasional large payloads.

If you look at what it takes to do cost-effective transportation beyond low earth orbit, of course you need to start reusing what I’ll call the earth departure stages—the rockets that post the payloads to earth escape have to come back. That’s not that technically difficult to do.

They then need to be refueled on orbit, so that they can be re-used. To do that you have to have a propellant storage capability on orbit, and I think one large consumer of launch for a long time to come will be propellant launched from the earth to those orbiting facilities.

I think people are going to be an important part of the traffic model going to orbit. For example I think that Richard Gariott’s time on the space station shows that there is actually a market for on-orbit labor, there are things for people to do on-orbit that pay.

It’s just that right now those things don’t pay as much as it costs to get the people up there.

But with a fully reusable system, you’re talking about a price point where very clearly the opposite is true. Flying people up to orbit becomes like flying people to an offshore oil rig or a research station. People do it because it pays to do it.

The third major segment is going to be that most of the things that we build in space can be effectively built in space out of modest sized pieces, hundreds of kilograms. And a system that can take a couple of people and payloads of that class will be needed and successful.

Launches like those are going to be so much cheaper to fly per kilogram than the large vehicles that fly less frequently. The only things you’ll fly on the large vehicles will be things that you can’t break into smaller pieces. For example the earth departure stages themselves, when they have to be replaced, will probably go up on large vehicles.

Now I hope XCOR is part of that transportation system, and it’s my job to try to get us there.

I have thought about if we get to the point where we are flying fully reusable orbital systems what do we do next. And I have given some thought to whether it would make sense for us to start doing circumlunar transportation.

Obviously there are other companies out there that have vertical landing technology that are better equipped than we are to start doing things like reusable lunar landers.

And as I’ve said publicly that once you start flying to the moon, if you care at all what it costs, you start producing propellant on the moon so you can refuel your ships, rather than carrying all the propellant from the ground and that dramatically reduces that cost.

Also, I’d love to see the beginnings of a Mars transportation infrastructure put together. It’s a technically very interesting problem and very doable, but it does require some R&D to do that cost effectively. And I have tried to do what I can to interest government agencies like NASA in doing that R&D so that cost effective transportation to Mars can be obtained one day.

BC: A couple final questions: How is the Midland migration coming along?

JG: It’s always in a forward direction. We continue to work with Midland on navigating our way through the FAA spaceport licensing process. We are going back and forth with the building contractor on hangar renovations. Certainly taken a little longer than I’d like to get the renovation plan hammered out.

We have some rented office space in Midland right now, about six folks working out there.

And they’ll move over with the rest of us, to the hangar, when we are ready to [establish the Research and Development / Flight Test Center in Midland].

BC: Any more updates on the spaceport licensing process?

It’s hard to say much more about that. What’s going on is that as the FAA continues to ask questions we continue to generate answers. At some point we think they will run out of questions. So far we have not run out of answers.

BC: In the meantime, how is XCOR coping with the existing space in Mojave?

JG: [laughter] We are very, very, very full. It’s a challenge. I eagerly look forward to the larger space.

BC: How would you say XCOR is different from the XCOR of 10 years ago?

JG: Maybe it’s just me but it doesn’t feel all that different. I still get my hands on the hardware, everybody still knows everybody fairly well. We still feel like a small shop, we’re still all in one location—it’s just bigger.

I don’t get as much time with each person as I used to and I can’t spend as much time talking at conferences and things like that, because I have too much to do here.

One other thought: After Lynx is flying, a lot more of our people are going to be by percentage in the non-technical parts of the company—in business development, in support of the wet lease operators, and in sales and marketing because they are going to grow significantly. But even then it is my hope that those essentially become divisions of the company and the engineering R&D shop keeps this tight-knit feel.

Next up: XCOR Chief Operating Officer Andrew Nelson talks business. You can connect with Andrew on Twitter as @XCORAndrew.

The story continues: Follow the build

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XCOR A&P Derek Nye prepares the inside of the Lynx Mk. I fuselage to receive the flight LOX tank.

Welcome back.

Over the coming year XCOR is developing its first spacecraft. And as one of our guys just said, this is the year of the Lynx. As discussed back in September we are taking you through that journey, post by post to first flight.

Next, we will kick off weekly coverage of all things XCOR—and Lynx—through a new Q&A with XCOR Chief Executive Officer Jeff Greason, touching on some of the big picture highlights of what to expect in the coming year, and recapping a bit of 2013.

We will then check in with XCOR Chief Operating Officer Andrew Nelson, and he’ll  provide both his view of the highlights and fill us in on any really cool developments on the business end. You can check out a recent interview with Andrew regarding space policy here.

After that we will connect you with our engineers and team to discuss Lynx status and the Lynx experience, and answer any questions you may have about XCOR.

Sit tight, everything is about to accelerate once more.

XCOR at AGU

13-01-08_khaki-3412-2_resizeToday XCOR begins a full week at the American Geophysical Union’s 46th annual Fall Meeting in San Francisco. We’re talking with Khaki Rodway, Director of Payload Sales and Operations, about the future of research opportunities onboard Lynx as they relate to AGU participants.

Khaki handles all research and education missions onboard Lynx flights. She is the “Your Mission. Our Ship.” side of the XCOR equation.

The XCOR team, including Khaki, will be at booth 245 from Monday, December 9th through Friday, December 13th. Please drop by and say hello!

You can also connect with XCOR and Khaki directly on Twitter.

Bryan Campen: So what is XCOR doing at AGU?

Khaki Rodway: XCOR is at AGU to deliver a glimpse of the emerging opportunities onboard Lynx for anyone involved with atmospheric science, planetary observation or space physics (for instance). These opportunities are new and provided through Lynx, our commercial suborbital vehicle.

So what I am doing this week is talking to scientists about the paradigm shift Lynx provides the AGU community.

BC: For the uninitiated, can you elaborate on that shift, and how Lynx connects with AGU participants?

KR: When it comes to space-based research and observation, scientists now have the ability to get into the field as never before, and get to where they want to go with Lynx.

BC: And what are the main advantages of Lynx for atmospheric scientists, planetary scientists and space physicists?

KR: It’s threefold: First it’s the ability to fly at low cost, which makes high flight rates achievable. Second, the fact that researchers can fly with their experiments will be a game changer. And third, the greatest advantage, the one that makes Lynx so exciting and beneficial to scientists, is that each flight can be entirely dedicated to the scientist’s mission–they don’t have to share their g-profile or pointing profile with other experimenters.

Scientists will be able to gather in-situ measurements at multiple points in the atmosphere or direct a telescope at a specific planetary object, for instance.

BC: Can you give some specific examples of how advances in suborbital space flights will change research and experimentation for the better?

KR: Sure. Take space hardware, where automation is the norm.

Before hardware is ever on orbit you have to know that it’s going to work. Because if it doesn’t work you can’t just go up there and fix it.

But if you can do your calibration tests with a human in the loop and fly frequently at low cost in a relevant environment, you can save yourself time and heartache by knowing that the instrument will work the first time it’s put on a satellite.

If something goes wrong with your hardware, your experiment, you’d like to get your hands on that hardware and fix it… but you can’t. After launch, there is no way to tweak and modify anything. Perhaps months later you’ll retrieve it.

Lynx is designed for low cost, high frequency flights. By comparison–take sounding rockets as an example. Much of the research conducted at this level of the atmosphere currently involves sounding rockets, and those are about ten times the price of a Lynx flight, maybe a few flights per year per experiment.

And this ability for Lynx to fly at such low cost and high frequency makes high flight rates achievable, which is what makes the whole future of suborbital research so attractive. With increased frequency, you have the opportunity to test equipment in-situ and know much more about what to expect well before launch.

With Lynx, we can dial up flights on a couple of hours’ notice, which matters a lot for anyone wanting to perform research at a pace that’s interesting.

BC: OK so that’s low cost and high frequency flights, and in-situ measurements for instrumentation development. How would Lynx be relevant to, for instance, an atmospheric scientist?

KR: Let’s say I’m a researcher who wants to gather data on noctilucent or polar mesospheric clouds. These clouds form spontaneously and hang around for several hours. With Lynx rapid call-up time—Lynx can be ready to fly in 2 hours—it can get me to 80 kilometers before the clouds disappear. That has not been possible until now. If the weather changes and I only have two hours to fly to 80 kilometers, I now know I can do that.

BC: So a researcher can have increased frequency with Lynx, and at a sharp decrease in cost from today’s offerings. What else?

KR: One of the most interesting opportunities on the horizon with Lynx is that Lynx can be used as a dedicated space-based research vehicle that flies a single scientific mission. Much like oceanographers and marine geoscientists have their ocean-going research vessels that go to their areas of investigator interest, Lynx can do the same for space researchers. Space scientists can get into the field, collect samples at a particular altitude in a particular part of the world, or look at specific object in the solar system or area of the Earth when and how they want.

It is my flight, “my” vehicle with a scientific mission.

BC: Last question: What is the “Ignorosphere”.

KR: The Ignorosphere is a phrase scientists use for the Mesosphere/Lower Thermosphere (MLT) region, which is at about 50 to 140 km altitude, and is likely the least sampled and understood region of the Earth’s atmosphere.

It’s the region of the atmosphere where all of this research will happen.

Scientists call it the Ignorosphere because it is above the region accessible for sampling by aircraft and balloons, and below the region of satellite access. Sounding rockets do get into the MLT, but they quickly pass through it.

Lynx is going directly into the MLT, which means scientists can examine up close transition zones such as the mesopause and turbopause, or Earth’s highest clouds known as Polar Mesospheric Clouds (PMC’s), or the regions where solar UV variability has its greatest impact. With Lynx floating in this region for several minutes, scientists now have the ability to do fine scale in-situ sampling of key chemical trace gases, meteoritic dust, isotopes of trace gas elements, water vapor, sulfates, CO2, just as an example. All this can be accomplished frequently, repeatedly, and at an extremely lower cost than existing platforms or capabilities.

 

Flight panel

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The Lynx flight panel is designed around a two-screen electronic flight instrumentation system. This system gives our pilots all the flight path and performance they require on the left screen and, on the right, all the information necessary to manage the engine and Lynx systems. Other instruments surrounding the main screens are present as backups. It is hinged around a center post and swings out for easy maintenance.

More on cockpit origins and progress in the coming weeks.

Pictured is an illustration of the final product in action at about 100 kilometers.

Tomorrow we cover slosh tests!

Stay tuned.

 

Listening

stethoscope 2

The propulsion system on Lynx is supported by a steel truss that attaches to the rear firewall of the fuselage. Composite blast shields surround each engine.

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In front of the engines, the truss supports all the valves, pumps, and plumbing needed to control and deliver fuel and oxidizer to the engines. In these shots, engineer Jeremy Voigt checks for small control line leaks using a stethoscope.

XCOR Piston Pumps – the Holy Grail

An XCOR rocket piston pump with colors so intense, it appears ready for the Fourth of July

Welcome back!

As we discussed recently, XCOR engines are set apart from the rest by their long life, reliability and reusability.

But they are also set apart by how they are pump-fed.

XCOR’s rocket piston pump simplifies the overall propulsion design versus traditional rocket engines. It lowers the overall weight of the vehicle by enabling the use of low pressure liquid oxygen and conformal kerosene tanks, and enables the quick turnaround of the vehicle since it enables “gas and go” rocket engine operations.

Usually high-performance rocket engines use turbo pumps that include complicated design features, extreme internal operating conditions (thus needing exotic materials), have limited (bounded) range of thrust once they are designed, and typically require extremely-skilled, highly-paid staff to produce and maintain the pump inventory. The typical life-span of a high performance rocket turbo pump today is about 30 minutes (sometimes less, sometimes more) before it renders itself unusable and in need of replacement. A good rocket turbo pump for an upper stage expendable launch vehicle will cost between $500,000 and several million dollars apiece.

By comparison, XCOR’s piston pumps require no exotic manufacturing processes or materials, and the component parts can be built by readily available high-precision machine shops. The pump may be serviced on a typical shop bench in under a few hours by a technical school graduate or junior grade FAA licensed Airframe & Power Plant (A&P) mechanic. The XCOR rocket piston pumps can then be mounted on a rolling test trailer, checked-out the same day and installed on the Lynx. The all-in purchase and assembly price is an order of magnitude less than a turbo pump of similar capability.

Our rocket piston pumps will undergo regular preventive maintenance as we check on internal wear and tear, replace seals, and ensure the pumps are ready for flight. XCOR believes that rocket piston pumps in use for Lynx will last hundreds if not thousands of hours, with regular preventive maintenance. And at three minutes per flight, this adds up to a lot of rocket flights!

Each piston pump can run at a different speed to supply different amounts of propellant for various engine outputs within a fairly broad range of thrust levels. They can also provide propellants for more than one engine at the same time.

For example, recently XCOR sought to increase the thrust of an engine by 30 percent. In the turbo pump world, that probably would have precipitated a completely new design of the turbo pump, including millions of dollars of non-recurring engineering and one to two calendar years of time. In our case, we had significant margin and just turned the pump speed up to achieve the desired thrust level.

In the Lynx, each pump is so powerful it can drive propellant for two (of the four) main engines with significant margin. In other words, one pump is so powerful it provides the liquid oxygen for two engines! And a second pump provides the fuel (kerosene) for the same two engines. This makes the baseline for the Lynx propulsion system four pumps and four engines. Each engine is roughly 3000 lbf of thrust.

Given all the advantages of the rocket piston pump above, one might ask why turbo pumps are ever used in rocket propulsion systems. For smaller thrust levels below 60,000 to 100,000 lbf of thrust (depending on the fuel, liquid hydrogen or kerosene, respectfully), we ask the same question. But above these thrust levels, the turbo pump output performance per unit of weight becomes an advantage over the piston pump.

In later posts we’ll discuss more about the propulsion system, piston pumps, and at a high level, the thermodynamic cycle that makes it all work.

Tomorrow we will show you a test article for the cockpit.

XCOR Lynx: Aerodynamics — Sub-sonic wind tunnel model assembly


Engineer Mark Street assembles a sub-sonic wind tunnel model Lynx, which was used at the U.S. Air Force test facility at Wright-Patterson Air Force Base near Dayton, Ohio.

In addition to computer modeling with computational fluid dynamics, wind tunnel models provide the necessary real-world data that together informs the final shape of the vehicle. We will cover all of these topics and more in the near future.

Tomorrow we cover some questions from the week, and update you a bit later on where you can find us on the road.

XCOR Lynx: Landing Gear 101 – Drop Tests

Lynx landing gear is carefully designed to be as light as possible while handling all possible load cases. Many tests are conducted to ensure the gear will withstand the forces involved. Here XCOR Engineer Brandon Litt prepares a Lynx landing gear prototype for a drop test. Over the coming weeks and months, we will show you more of the process around landing gear development.

Tomorrow we’ll show you a shot of the Lynx subsonic wind tunnel model. It’s pretty awesome, look for it at 9am PST.

XCOR Lynx: Cockpit engineering model

Before creating the final cockpit, we first made a full-sized engineering model to help us engineer its various sub-systems including avionics, life support, ingress-egress, seat hardware, payload locations and more. This model was pulled from a mold that was also used to make the final item.

In this photo, the engineering model of the Lynx cockpit has just been pulled from its mold, which sits upright and partially obscured by the tarp on the left.

It’s all about the gear on Wednesday. Stay tuned.

Build a little, test a little


XCOR’s Derek Nye and Ray Fitting prepare the Lynx truss for a test day.

XCOR follows a rapid design-build-test approach to developing new products and systems critical to the success of all XCOR programs. We excel at the fast hardware design, build and test of non-toxic liquid propulsion systems. This includes our Lynx main engines, as discussed last week. While non-toxic systems are critical to the overall safety of the Lynx system, they are also vital to the low cost of operation and ownership of Lynx.

“Build a little, test a little”

This “build a little, test a little” approach allows for many Lynx concepts to be evaluated, physically validated and changed rapidly using inexpensive and practical analysis and test methods, rather than relying solely on costly and time-consuming modeling and simulation. It also allows for other projects to generate serious results.

For example, other programs have received multimillion dollar contracts to study pumps without building any hardware. Eventually, a pump may be produced for many more millions of dollars. On the other hand, over a period of 2 years and at dramatically less cost, XCOR has worked with ULA to produce a working liquid hydrogen pump that demonstrates convincingly that it will work for a similar-sized engine with much higher reliability and reusability, and again, at far lower cost. Such outcomes are possible due to frequent and routine testing followed by fast iterations. This produces truly innovative results, and a serious increase in safety and reliability.

When fast iteration is pursued, XCOR focuses on critical operational parameters and requirements for propulsion such as low production costs, ease of maintenance, long life, full reusability and long term producibility. For long-term producibility, we are designing to anticipate the related techniques, materials and processes that may be readily available 20 to 30 years from today.

There are further critical elements, and by focusing on these parameters we drive down total cost of ownership of our systems through upfront procurement cost, maintenance man hours per flight, vehicle turnaround time, life of the product, cost of replacement parts, and reduced support crew and equipment. This positive feedback loop is a benefit to our customers, but also enables enhanced safety. The lower cost of the system to operate, the more that system may be flown. The more it is flown, the more we learn. And the more we learn, the safer we can be.

Design-build-test and XCOR culture

Mobile test stands also feed into our approach. With only minimal fixed test infrastructure at remote locations, we eliminate the need for separate crews reporting to different parts of a larger organization. This fosters a unified design-build-test culture in our company. All equipment and personnel return to the hangar at the end of each test day. Propulsion systems under test are worked on in the comfort of the hangar with all tools and personnel available, then taken to the nearby test site. All engineers and technicians work together toward the common goal of a working product.

Nothing is duplicated, we are one team, costs are contained and safety improves yet again.

Tomorrow: The importance of an actual Lynx cockpit engineering model