Wednesday, June 22, 2011

Commercial Asteroid Return to Station

Back in 2010, Michael Mealing began to consider a spacecraft mission to capture and return a very small Near Earth Object (NEO) to the ISS or Bigelow module for study. He writes about business concept here. Michael’s point, humanity will only travel into the solar system if they can make money at each step. NEOs may be the next step after LEO.

Then in January, 2011, the topic of a NEO capture and return to LEO comes up again in the comment discussions on the Space Business Blog here. So Michael and I have teamed up to continue refining this business concept.

Here’s a Pencast describing the basic concept for a mission to return a small asteroid sample to a space station in LEO.  I also include a few markets that might make such a mission profitable.

brought to you by Livescribe


Moon dust legally for sale - $50K for a few small specs. 

Next, I will walk you through the spreadsheet model built to analyze what would be required for a mission like the one described in the Pencast above.

Assumptions:
  1. Spacecraft launched to LEO Space station to standby until target asteroid has been identified.
  2. Spacecraft launched from LEO space station and returning to LEO space station.
  3. Haul all propellant for round trip (no refueling).
  4. A duplicate amount of Delta-V will be required for both the trip out to the asteroid and the trip from the asteroid back to a LEO space station (assuming NO aerobraking to avoid damaging asteroid). Note: The mission’s costs could be greatly reduced if one could determine a smart engineering method to reduce the needed delta-v for the return trip to a LEO space station.
  5. Mass of dry spacecraft: 200Kg (Similar to NEAP but swap out all of NEAP's science gear for some type of grappling mechanism).
  6. Engine efficiency Isp = 342 seconds.
  7. Although spacecraft is docked to LEO space station before mission start, this model assumes no propellant boil-off or LOX top-off prior to mission start. 
  8. Since the target NEO is still undetermined, multiple Delta-V’s were modeled to reach NEO targets. Delta-V’s between 5500, 4500, 3500, and 2500 m/s were considered.
  9. Asteroid 2010 RF12 has a radius of 3.5m and a mass of 500,000kg according to NASA. Prorating these values to a radius of 0.5m gives you a sphere slightly smaller than the desired “refrigerator” in Michael Mealing’s earlier posts with a mass of 71,429Kg. This mass is larger than what I wanted to consider for a proof of concept mission, so although I include the 71K Kg mass in the analysis, I focus on target asteroid masses of 500, 300, 100, 50, 25, and 10Kg.

Conclusions:
The table below is the summary of my analysis. The columns in the table below represent the multiple delta-v’s modeled for our 200Kg spacecraft to travel from a LEO space station and AR&D with the target NEO. The rows are the various NEO masses that were considered (or – how big of a rock the mission can go out and get). The data populated (the cells with numbers) are the total mission masses for each combination of delta-v and NEO mass. The total mission mass includes all propellant needed not only to reach the NEO but to return it to LEO as well. The color coding correlates to the launch vehicle table below – Dnepr in green, Falcon 9 in orange, and Falcon Heavy in purple.






















A few Observations:
  • Finding low delta-v targets will dramatically increase the size of the asteroid one could successfully return. For example, instead of a 10Kg target at 5,000m/s of delta-v, the same spacecraft could return a 500Kg target if only 2500m/s of delta-v were needed to reach it (and at almost half the total mission mass!) – that is a lot more rock for scientists to analyze – 500kg instead of 10kg.
  • Are there ways to decrease the delta-v required to reach these targets or return from them (currently avoiding aerobraking, but maybe a small asteroid could be shielded during aerobraking)?
  • Because such small NEO objects will be difficult to spot a head of time (there are many more NEOs than we have on record - especially small ones), such a mission has to be very patient waiting on station many months/years for the “perfect” NEO to approach with the right blend of low delta-v and a mass that is “just right”. And to respond to new targets, the mission must be ready to depart the station on very short notice in pursuit of any newly identified targets.
  • Growing humanity’s knowledge of very small NEOs increases the chances of mission success.

Here is an example of the tables I built to analyze propellant needs. Here are the tables feeding the 5500 m/s of delta-v column. The colored cell in each table varies the asteroid masses. Here is the interactive spreadsheet for those that want to modify my assumptions and want to view the tables for the delta-V's modeled as well.

Delta-V 5500m/s:




































Next steps:
Michael and I plan to refine this concept over the coming months. Look for follow-up posts here on SBB and over on Michael’s blog.

Tuesday, May 31, 2011

Business Case for a CubeSat-based Earth Imaging Constellation

The use of Commercial Earth Imaging Satellites is growing. Individuals, corporations and governments are finding varied and unique applications for images of our planet.

Futron estimates the market for commercial earth imaging topped $1B last year (2010).


Uses of Earth Imaging:
  • Disaster Relief – think of all of the satellite images you saw after the Japan Earthquake (including the nuclear reactors)
  • Disaster avoidance - George Clooney (among others) paying to patrol boarder of north and south Sudan using Earth imaging satellites.
  • Helped with hunting down Osama bin Laden (but were any these images from commercial satellites?)
  • Food Commodities tracking – allowing traders to ask and answer questions like, “how do the wheat crops in Kansas look after last night’s hail storm?”
  • Remote Infrastructure observation – the oil industry uses it to keep track of their assets in remote locations
  • Even the US Government is turning to Commercial providers. Last year, the U.S. National Geospatial-Intelligence Agency (NGA) awarded separate 10-year, $3.5 Billion contracts to image providers DigitalGlobe and GeoEye (these contracts are now under review).

The Commercial earth observation markets:
  1. Market #1: High-Resolution images (1.5 meters per pixel). But the cost of each satellite means providers have a limited number of satellites (usually 1-2) on orbit.
  2. Market #2: Med-Resolution images (5-7 meters per pixel) – lower quality images, but providers tend to have more satellites in orbit and may offer more spectral bands to choose from for each image and offer more frequent photo opportunities due to the higher number of satellites within the constellation.




















In a recent Nov 2010 paper, “6U CubeSat design for Earth observation with 6.5m GSD, five spectral bands and 14Mbps downlink,” author, Dr. Steven Tsitas outlines how a constellation of 6U CubeSats could serve Market #2 (frequent med-res images) competitively. (Sorry, I think you will have to buy the paper. If a reader finds a free version of the paper online, let me know and I will change the link). I hope to post an interview with Steven Tsitas soon.

But why even consider a CubeSat at all for such a mission? Here are just a few of the advantageous of using CubeSats:
  • High amount of innovation in the field – from NASA, universities, and private industry
  • Low ITAR restrictions (CubeSat programs are thriving in many nations)
  • Low mass of each satellite
  • Reduced launch cost per satellite
  • Reduced cost to replace/upgrade constellation as satellites age, breakdown, or new technology becomes available

Rapid Eye, a German company, is the current leader serving Market #2. Below I will provide some details about Rapid Eye and how a CubeSat constellation might be able to compete with Rapid Eye.  First, a little education about Rapid Eye.

Rapid Eye Details:
  • Five identical sun-synchronous Earth observation satellites
  • Five spectral bands
  • Launched in August 2008
  • Satellites built by Surrey UK
  • 650KM circular orbit
  • Captures 4mil km squared of earth’s surface every day
  • Once an order is placed for an image, can take a photo of any location on earth (between 75 degrees N and 75 degrees S) within 24 hours.
  • Offers not only images, but offers services for the analysis of images – especially good at providing comparative analysis of images taken over a period of time

Rapid Eye, the Numbers:
  • Customer price for images: $1.33 per square KM (must purchase 5,000 KM at a time (at current Euro conversation rates that is equal to $6650 per very large image)
  • Satellite Constellation construction: $35M 
  • Expected 2009 Revenue: $29.5M (have not confirmed this number)
  • Total Capital needed to break even: $224M

Assumptions about Rapid Eye’s business:
  • Assumed Rapid Eye is now profitable
  • Assumed the cost of the single Dnepr launch necessary to lift the five Rapid Eye sats: $15M
  • Assumed a $50M infrastructure Hardware purchase (ground station and other startup infrastructure)
  • Assumed a five year startup at a cost of ~$25M per year in operating (non-HW, non-infrastructure costs)













So what if we could launch a constellation of ten cubesats that could perform a very similar function as Rapid Eye’s current constellation of five small sats? Are their savings if we could? For this post, I will use Steven Tsitas’s conclusions that, yes, such a cubesat constellation would be technically possible.

I will build my business case, not from a technology discussion, but by attempting to answer the business question of - how much could an business save by using Cubesats instead of small sats?

CubeSat Venture Assumptions:
  • Cost per 6U CubeSat: $400,000
  • Number of CubeSats in constellation: 10
  • 6U CubeSat mass: 8 lbs each
  • Falcon 1 launch: $9.8M
  • SpaceX willing to prorate launch cost based on mass

If we assume the CubeSat venture would operate using the same Hardware and Operating Costs as the Rapid Eye venture, then the CubeSat savings are limited to the cost of the satellites themselves and the cost to launch them into orbit:
  • Rapid Eye’s satellite and launch costs: 23% of breakeven costs
  • CubeSat venture’s satellite and launch costs: 3% of breakeven costs
This would mean a CubeSat venture competing with Rapid Eye could theoretically lower image prices by twenty percentage points over competitors (all other things being equal). This by itself may close the business case for some CubeSat constellation investors.











But perhaps competing toe-to-toe with Rapid Eye is the wrong business model. As a general rule, it is hard to out Wal-Mart, Wal-Mart. What-if the CubeSat earth imaging venture could, instead, become the low-price, no frills, earth imaging provider?

In the earlier example, the CubeSat advantage was limited to lower satellite costs and cheaper rides to orbit on SpaceX launch vehicles. But what-if the venture could also save money on ground costs: Hardware/ground stations and operating expenses?

CubeSats, the low-cost leader in earth imaging Assumptions:
  • Continue with assumptions regarding low satellite costs
  • Continue with assumptions regarding low launch costs
  • Lower ground Hardware and Infrastructure costs from $50M to $25M
  • Lower operating costs from $25M to $10M per year.









Here is a quick cost comparison between the options:


















Next Questions (beyond the scope of this post):
  • Market price elasticity: How price sensitive is the earth imaging market? How would cutting Rapid Eye’s price by 20-60% affect demand for a CubeSat-based image product?
  • What realistic cost reduction methods are possible in ground hardware and personnel?
  • Admittedly, my Rapid Eye information was limited to publicly available data, a more serious effort should be conducted to understand the competitor’s cost structures and current profit forecasts
  • What are the cost implications from using a CubeSat-based system? Where are system costs reduced? Where are system costs increased?
  • Admittedly, images from a CubeSat are of a lower quality than the best in orbit (5-7 meters per pixel compared to 1.5 meters per pixel from the industry leaders of market #1).  How sensitive is the market to image quality?  And what can be done to increase the quality of an image taken on a 6U CubeSat?

Sunday, May 22, 2011

Interview: Alan Wasser & Space Property Rights Textbook

The National Space Society posted last week about a new Law School text book that includes a chapter on space property rights written by Alan Wasser and the Space Settlement Institute.

I first interviewed Alan Wasser a year ago and later built a business case on a lunar facility operating under Alan’s proposed land claims legislation.

With the release of the new textbook, I wanted to catch up with Alan so he could give you an update:



Q. For those that don’t know, what is "Land Claims Recognition" and how does it relate to space property rights?

Alan Wasser: There is one very high value, zero volume product that already exists in space, just lying around waiting for us to exploit it: Real Estate.

Land Claims Recognition would allow private Lunar settlements to claim some Lunar real estate and sell portions to people back on Earth, serving as a revenue source to fund private enterprise space settlement. No need to set up a factory in space, No need to mine it. No need to haul it back. Just land, set up a permanent settlement, claim it, and start selling the surrounding land to investors and speculators back on Earth to pay back the cost of developing affordable transport.

The US government has now officially decided not to go back to the moon, philanthropists cannot afford it, and there is nothing else on the moon or Mars that could be profitable enough to justify the cost of private enterprise developing safe, reliable and affordable human transport.

Therefore, Land Claims Recognition is now clearly the only way we are ever going to see a significant return to the moon, but this time to stay.


Q. You provide a legal defense of these land claims. Talk to me about your efforts.

Alan Wasser: Land Claims Recognition would allow individuals or companies to appropriate and sell lunar land, - but ONLY after they have already established a true permanent human settlement on the land they are claiming.

It is the settlement, itself, (and only the settlement) that can make a claim under the Outer Space Treaty. No Earth government can claim the land or give it to them. The only thing governments can do (or not do) is pass laws about how their courts should treat sales of Lunar (or Martian) property to their citizens - "recognizing" the legitimacy of the settlement's claim and therefore, the validity of the sale.

When I started this debate, some argued that I was wrong about the legality of land claims recognition under the Outer Space Treaty, etc. So Doug Jobes and I took the time to establish an airtight legal case for it. In its winter 2008 edition, SMU Law School's "Journal of Air Law and Commerce" published our article describing land claims recognition in detail and establishing the legal basis for it, complete with 182 footnotes. The Journal is the oldest scholarly periodical in the English language devoted to the legal and economic problems of aviation and space, and is the most prestigious law journal in its field.

You can read the article here. For a less legalistic version of how Land Claims Recognition work (and the answers to 25 frequently asked questions) see here.


Q. And now Land Claims Recognition has been included in a new law text book?

Alan Wasser: Yes! The fact that lunar land claims will now be taught in law schools is an even more convincing demonstration that, though there may always be some dissent, the general legal community seems to have accepted Land Claims Recognition as being fully in accord with existing international law.

The textbook is from Westview Press: "International Law", Silverburg, ed., (ISBN 978-0-8133-4471-3). "Space Settlements, Property Rights and International Law: Could a Lunar Settlement Claim the Lunar Real Estate It Needs To Survive?" is Chapter 13, pages 275 to 299.


Q. When we last spoke, you were marshalling an effort to approach Congress with legislation consistent with your articles. What is the status of your legislation?

Alan Wasser: The AIAA Space Colonization Technical Committee (SCTC) recently sent two teams to Congress to lobby for a Land Claims recognition law. They got a good reception but no comittments. It will need much more support from the Space community to actually get introduced and passed, setting off the next space race.



Space Business Blog Footnote and full disclosure: Over the last year I have become more and more convinced by the mission of the Space Settlement Institute, so earlier this month I joined their volunteer staff as a policy analyst.

Friday, May 20, 2011

Creating Culture at a Commercial Space Company

“If you want to build a ship, don’t drum up the people to gather wood…Instead, teach them to yearn for the vast and endless sea.”       -Antoine De Saint-Exupery, Author of The Little Prince

When young entrepreneurs talk to me about starting companies – I encourage them to articulate what they want the culture to look like five years from now. Culture is a sneaky thing…it always gets developed. No company lacks a culture, but many lack good ones!

The Netflix culture is well articulated in the slidedeck below (by Reed Hastings, Netflix's CEO) - fastest 128 slides you will ever read. Well worth every slide! Now aerospace companies won’t be able to leverage all of these ideas – especially Netflix’s policies and procedures on “policies and procedures”, but Netflix has intriguing ideas that many new space entrepreneurs will benefit from:
  • Hiring the best (to minimize the need for written procedures)
  • Keeping only the passionate people (see the opening quote)
  • Take as much time off as you want (if you love what you do, too much vacation won’t be a problem)



Tuesday, May 17, 2011

Altius Space Machines: Sticky Boom Markets

Jon, Mike, and Forrest of Altius Space Machines stopped by my house after their successful Zero-G flight.  I only got a few hours with them, but I did get to see (and touch) their current "Sticky Boom" prototype.  Below is my pencast (from LiveScribe) based on conversations with Altius founder, Jon Goff. 

In addition to a summary of the technology, the pencast discusses three potential Sticky Boom markets:
  1. Cleaning up space debris
  2. Enhancing science missions
  3. Enabling micro-cargo delivery to space stations





And for those that missed it, here is ASM's highlights from Saturday's Zero-G flight.

Monday, May 16, 2011

NASA's Commercial Crew/Cargo Market Assessment

NASA has released a 40-page Commercial Crew/Cargo Market Assessment for Low Earth Orbit.  RLV News pointed me to the softcopy – thanks Clark.

Here is NASA’s summary of the next ten years of projected commercial demand for cargo and crew to Low Earth Orbit (LEO) with commercial demand ranging from 7K-60K lbs of cargo and from 44 to 360 commercial astronauts.


Here are the Nuggets from NASA's assessment I found especially valuable:
  • Crew Transportation drives the overall market.
  • 4 Commercial Crew/Cargo Markets: (1) Countries lacking Space Programs, (2) Space Tourism, (3) Applied Research, (4) Other Markets – Satellite Servicing, Media, Education
  • Report looked at a ten year time horizon
  • Report excluded NASA Crew/Cargo usage - commercial usage only
  • The average ISS crew member uses 10.3 lb/cargo per day (based on historical NASA/Russian usage)
  • 4 Space Tourism Growth Constraints: (1) Crew Transport Availability, (2) Cost per customer, (3) lack of destinations besides ISS, (4) long training time
  • ISS’s Upmass Requirements 2011-2020 = 318K lbs: (1) Core Systems/Operations = 194,820 lbs, (2) Funded Research = 80,067 lbs, (3) National Lab Utilization (unfunded) = 43,266 lbs
  • Current ISS limitations as a research platform: (1) Inadequate HW/instruments to support research, (2) lack of frequent and affordable up/downmass to/from ISS
  • Report concludes that availability of up and downmass is “a major constraint to development of the market” and quotes the National Research Council as saying, “conditioned down mass of particular importance…”
  • Current research on ISS: Basic Research. Over next ten years, ISS research will gradually shift to governments paying for proof of concepts and private ventures pursuing commercialization of successful proof of concepts.
  • NASA is on contract to purchase 132K lbs of ISS cargo through 2015. According to the authors, NASA ISS cargo demand from 2016-2020 is currently flat for another 132K lbs
  • 4 Classes of Research conducted on ISS: (1) Biology/Biotech – 70% of ISS research to date, (2) Earth Observation, (3) Physical/Material Sciences, (4) Technology Development/Space Qualifying
  • United States does 36% of the research on ISS
  • But only 9% of all research on ISS to date is “Commercial” in nature – and even this “commercial” research to date has been subsidized by non-commercial sources.





Comments:
  • Although not presenting very much new data, the authors confirmed and consolidated a significant amount of commercial market data into one place
  • The authors relied heavily on industry values to determine the upper end of these markets.
  • The authors never exceeded industry's optimism.  The authors in every case established low end demand by extrapolating from history.
  • Although mentioning the critical importance of downmass to station research, the authors did not provide a downmass demand estimate for the next decade
  • I look forward to the day when commercial research on orbiting stations far exceeds the current 9%!
  • Overall, a very helpful report (if, perhaps conservative) that will stay on my shelf as a reference.

Thursday, May 5, 2011

XCOR's Nano Sat Launcher

At Last Week's Space Tourism Society’s +10 Dinner, I spoke with two of the founders of XCOR: Aleta Jackson (Co-Founder/Chief Technician), and Dan DeLong (Vice President/Chief Engineer). We discussed general Lynx status, customers, regulation concerns for each flight, XCOR’s preference to fly out of standard airports, etc. And then we changed gears to discuss the Lynx’s “Dorsal pod” intending to ride a top of the Lynx.

Here is an image of the Lynx without the Dorsal pod – in tourist configuration (my term).



Here is an image of the Lynx with the Dorsal pod on top – in NanoSat configuration (again, my term).



















XCOR’s stated plans are to develop an upperstage that can ride inside of the Dorsal pod to launch Nano-Satellites.  the Lynx would act as a first stage to get to 100km and the upperstage would take the payload to orbit. Here is an XCOR image of an upperstage launching out of the Dorsal Pod carrying a nanosat on board (perhaps my favorite XCOR image ever).



















Here are a few of the XCOR Upperstage specs:
  • 76cm diameter
  • 340cm long
  • Mass up to 650kg
  • 12kg Nanosat Payload
  • 400km circular orbit

This discussion with XCOR’s founders got me thinking again about NanoSat launches themselves. The small payload market (which include nanosats) can be segmented by how time-sensitive their launch is:
  • Low Time Sensitivity: Traditional NanoSatellites – a delay of a few days/weeks would be frustrating, but par for the course with rocket launches.
  • High Time Sensitivity: Urgent NanoSatellites perhaps fulfilling an ORS mission for the military of disaster relief
  • High Time Sensitivity: Package delivery to space stations – daily milk runs – fresh apples – critical (but small) replacement parts








I have said before how I believe package delivery to station to be a large portion of this “small payload” market because of the frequency of needed launches and ridiculously low integration requirements (how long does it take to load a bag of apples into a “no bruising” canister for launch?).















Now XCOR has a long way to go. A lawyer friend of mine reminded me last week when I was discussing this topic with him, “Yes, but XCOR has not flown their version 1 vehicle to altitude yet.” And he is right. The NanoSat launcher from a Dorsal Pod would be a Version 2 vehicle (at least), but…

…If I was to build a business to serve the small-payload-to-LEO market, I would want to secure a method to reach LEO as frequently as my customers needed. XCOR through their Lynx/Upperstage vehicle would provide an attractive solution if they can truly fly as often as they say they will be able to. It would not surprise me that, in the end, the market leader will be the company who can fly the most.

Monday, May 2, 2011

Space Tourism Society’s +10, Turning a Family into an Industry

On Thursday I attended Space Tourism Society +10 event in Los Angeles, CA. Dennis Tito, Space X, Virgin Galactic, 62 Mile Club and others spoke. This was less of a Commercial Space conference for those familiar with the feel of Space Access or Space Frontier Foundation’s NewSpace Conference. Instead this was more of a Dennis Tito-focused celebration of how far space tourism has come over the last ten years and what is to come in the next ten years.

What surprised me was the diverse audience at +10. I spoke with Alan Stern before the event.  He commented on the high percentage of new faces in attendance. During the pre-meal reception, I spoke with:
  • entertainment executives,
  • real estate investors,
  • lawyers, and
  • Virgin Galactic customers undergoing centrifuge training.

The event taking place in LA partially accounts for the diverse attendance list. But when John Spencer, event organizer, gets on the front page of the USA Today (above the fold) talking about Space Tourism, you know Times: they are a-changin. For those close to the New Space community, be ready for "the growing of the tent". For those new to Space Tourism, New Space, Commercial Space, etc. – welcome!

I expect over the next years, investor (and customer) interest in the sector will continue grow at the expense of that “family reunion” feeling we get at current new space gatherings. This is healthy: the family is growing into an industry. And it looks like an industry more and more each day. The Space Tourism Society’s +10 even is only the latest indication.

Sunday, April 24, 2011

Jeff Greason at TEDxSanJoseCA

Thank you Jeff.  Jeff Greason eloquently explains "Why Space?," and "Why do we need a frontier?"  I especially love this quote...
But the most important element of a frontier is psychological, because it is hard to sustain that believe in limits - that belief in the zero sum game - when you can see, stretching before you, new lands - untamed, untapped.  
I don't think it is an accident that the industrial revolution coincided with the age of sail.  I don't think it was an accident that the United States was founded on the edge of a very sparsely populated and untapped continent.  And this time, the lands that we see are truly unpopulated.  They are waiting for the gift for life.  ~Jeff Greason

Monday, April 18, 2011

Planned Daily Updates from Altius Space Machines

Remember the days of reading the Armadillo updates every Monday?!  I miss that level open communication by a New Space company.  I know some of Armadillo's customer's prevent them from sharing everything, but I enjoyed feeling a part of Armadillo's efforts each week.

That is why I am excited that Altius Space Machines just announced an intense effort to mature their "Sticky Boom" docking tool.  And through that "sprint" as they call it, Altius intends to blog daily on their progress - good or bad - words or pics or video.  Their website makes it sound like a pretty aggressive development schedule to develop their "Sticky Boom".

The Altius website described Sticky Boom as a long boom with a sticky pad on the end that can:
get meaningful adhesion to almost any material imaginable. Plastic, metal, rock, ceramic, MLI or MMOD blankets. Flat surfaces, curved surfaces, multi-faceted surfaces, completely random surfaces like NEOs. Even dust or regolith for that matter. You get all of the “contact at a distance” benefits that Kirk and Joseph Bonometti talked about, while also enabling secure connection with “non-cooperative” objects like uncontrolled satellites, Mars Sample Return sample canisters, space junk, and even asteroids or comets.
Altius says they have one month to get a Sticky Boom prototype ready for a ZeroG micro-gravity flight in May 2011.   This "sprint" should be fun to watch.   Good luck Altius Space Machines - we are cheering for you.  Follow Altius's Sprint here.