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Archive for October, 2009

Masten – Final Flight Attempt – Grumman Lunar Lander Challenge

Posted by drdave on October 30, 2009

Xoie

Xoie Ready. Credit: Ustream Screen Shot

We are watching Masten’s Xoie attempt at the Mojave site, live via Ustream.

The window began at 9:00 AM PDT this morning. Ready for flight at 10:16 AM.

First flight ended successfully after 3 minutes and 2 seconds. Masten is now preparing for the return flight.

It is now 11:04 and loading of LOX is underway.

Launch. 9 Minutes left in the window. Good Flight. Landed. Now its up to the judges.

The accuracy for Xoie’s first flight was around 11 inches (28 centimeters). Based on unofficial measurements, it appears as if Xoie did well enough on the second flight to take the top spot away from Armadillo’s Scorpius (average landing accuracy was about 35 inches – 89 centimeters). And indeed that is the Case. Level II Prize – Xoie First, Scorpius Second. And for Level I Prize – Scorpius First, Xombie (Masten) Second.

Jonathon Goff, found often on forum.nasaspaceflight.com, built the 1000 lb thrust engine, and Ian Garcia, guidance engineer, wrote the software.

Xoie

Xoie Ignition. Credit: Ustream Screen Shot

Xoie

Xoie Climb to Altitude. Credit: Ustream Screen Shot.

Xoie

Xoie Hovering Over Target. Credit: Ustream Screen Shot

Xoie

Xoie Landing After First Flight. Credit: Ustream Screen Shot.

Xoie

Xoie Refueling. Credit: Ustream Screen Shot

Xoie

Xoie Second Flight. Credit: Ustream Screen Shot.

Xoie

Xoie Descending on Second Flight. Credit: Ustream Screen Shot

Xoie

Xoie Second Landing. Wins!! Credit: Ustream Screen Shot.

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Ariane 5 – 29 October 2009

Posted by drdave on October 29, 2009

Ariane Launch

Ariane V Launch. Credit: European Space Agency – Arianespace

The sixth Ariane 5 flight of 2009 carried the first satellite launched by Arianespace for Telenor Satellite Broadcasting AS – THOR 6, along with the 32nd spacecraft from the SES group of companies. The previous Ariane 5 mission was October 1 with the Amazonas 2 and COMSATBw-1 satellites.

The THOR 6 is a 3,050 kg satellite fitted with 36 Ku band transponders for direct-to-home television services from Telenor Satellite Broadcasting to Central and Eastern Europe as well providing additional capacity in the Nordic region.

The NSS-12 spacecraft was produced by Space Systems/Loral and weighs 5,620 kg. It carries 40 C-band and 48 Ku-band transponders. This satellite will also provide direct-to-home television services from SES WORLD SKIES. The audience is in Europe, the Middle East, Africa and Australia.

Posted in European Space Agency, Rocket, Satellites, Space, Technology | Tagged: , , , | Leave a Comment »

Lunar Exploration Summer Intern Program 2010

Posted by drdave on October 28, 2009

2010 Summer Intern

The 2010 Lunar and Planetary Institute 10 week Summer Intern program. Evaluate possible lunar landing sites for robotic and human missions. The program is for Graduate students in Geology, Planetary Science, and related programs.

Posted in Human Exploration, Moon, Mars and beyond, Robotic Exploration, Space Exploration | Tagged: , , , | Leave a Comment »

Ares I-X – Second Launch Attempt

Posted by drdave on October 28, 2009

Following yesterday’s scrub, Ares 1-X survived the overnight thunderstorm and is scheduled for launch this morning. And we are watching on NASA – TV. Currently, they are reviewing systems within Ares I-X to verify there has been no damage. The nearest lightening strike was 700 feet (200 meters) away. The countdown is sitting at T minus 4:00 minutes, and launch is tentatively scheduled for around 9:00 AM EDT.

The resumption of the count is expected in about 25 minutes.

Ares 1-X Second Attempt

Ares I-X. Second Attempt. Early Morning Credit: NASA TV.

Second Attempt.  Hold for Rocket Check.

Second Attempt. Hold for Rocket Check. Credit: NASA TV.

Currently waiting for completion of the systems checks on Ares I-X and the weather. The main weather problem is “triboelectrification”, which is fully explained in this review of yesterday’s launch attempt. Briefly:

According to the 45th Weather Squadron of the Air Force – the Squadron responsible for monitoring all launch weather rules – Triboelectrification is defined as: “triboelectric charging observed to put aircraft and space vehicles into corona when they fly through clouds containing ice or precipitation in either phase.

“The corona generates radio signals known as P-static (Precipitation static). P-static can degrade the signal to noise ratio of critical communications to the vehicle, especially including the range destruct command link.

The new launch time is 11:00 AM EDT. Weather is expected to have an 80% chance to be acceptable at that time (8:00 AM Phoenix time).

Pad 39B

Pad 39B. Credit: NASA TV.

Aerial View of Ares I-X

Aerial View of Ares I-X. Credit: NASA TV.

If today’s launch is scrubbed, the next window is late December or early 2010.

With 20 minutes to go until 11:00 AM EDT, the launch director has polled all systems and all systems are ready for launch. Everything is ok except the weather for triboelectrification.

At 11:03, weather is no go and the estimate is for 20 to 25 minutes from now. And now, they plan to pick up the clock at 11:16 AM and launch at 11:20 AM.

At 11:20, we have a ten minute window. Launch Director looking to resume the count at 11:27 EDT.

The count has resumed with launch expected at 11:30 AM.

Launch success.

Ascent

Ascent. Credit: NASA TV.

More details.

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The Augustine Commission – Final Report – Hits and Misses – Part 3

Posted by drdave on October 27, 2009

(Part 1. Part 2. Part 3. Part 4. Part 5. Wrap Up.)

In Part 1, we looked at the pieces strewn about our living room floor. In Part 2, we examined the Goals and Destinations in Chapter 3.0.

Chapter 4.0 Current Human Spaceflight Programs

The current U.S. human spaceflight programs are the operational Space Shuttle Program and the U.S. portion of the International Space Station (ISS). The next human spaceflight effort, the Constellation Program, is in development.

4.1 The Space Shuttle

The Commission reviewed long history of the Space Shuttle, its two fatal accidents, and the increasing complexity of missions, especially those since the return to flight in 2005. Early missions were 4 to 7 days and rarely involved a space walk. Current missions are 13 to 14 days and have involved as many as 5 space walks. The Hubble repair mission is typical.

The Shuttle was scheduled for retirement in 2010, and the replacement vehicle was scheduled to arrive in 2012. After four years of development, the Constellation Program does not expect this replacement vehicle to arrive before 2016, at the earliest. Currently, the time between Shuttle missions is averaging 100 days. With six missions remaining, the schedule calls for completion in 2010, an average of only 64 days between flights. The schedule would extend into the middle of 2011 if current prudent safety practices are maintained.

The Committee explored three scenarios for the Shuttle:

  • Scenario 1: Prudent Shuttle Fly-Out. As noted, the current Shuttle schedule has little or no margin remaining. Scenario 1 is a likely reflection of reality. It restores margin to the schedule, at a flight rate in line with recent experience, and allocates funds in FY 2011 to support Shuttle operations into that fiscal year. Based on historical data, the Committee believes it is likely that the remaining six flights on the manifest will stretch into the second quarter of 2011, and it is prudent to plan for that occurrence and explicitly include the associated costs in the FY 2011 budget.
  • Scenario 2: Short-Term Support for the ISS. Space Shuttle retirement will have an impact on the ISS (described more fully in a subsequent section). Scenario 2 would add one additional Shuttle flight to provide some additional support for the ISS and ease the transition to commercial and international cargo flights. It could enhance early utilization of the ISS, offer an opportunity for providing more spare parts, and enable scientific experiments to be brought back to Earth. This additional Shuttle flight would not replace any of the planned international or commercial resupply flights.
  • Scenario 3: Extend Shuttle to 2015 at Minimum Flight Rate. This scenario would extend the Shuttle at a minimum safe flight rate (nominally two flights per year) into FY 2015. Once the Shuttle is retired, the U.S. itself will no longer have the ability to launch astronauts into space, and will have to rely on the Russian Soyuz vehicle. That gap will persist until a new vehicle becomes available to transport crew to low-Earth orbit. Under the current program, the resulting gap is expected to be seven years or more. This scenario, if combined with a new crew launch capability that will be available by the middle of the 2010s, significantly reduces that gap, and retains U.S. ability to deliver astronauts to the ISS.

While the Commission strongly leans toward scenario 1, it acknowledges good reasons for scenario 3, since American access to the International Space Station (ISS) and material support of the ISS are very important.

4.2 The International Space Station

Construction of the International Space Station was begun in 1998 and was scheduled to be completed with an aggressive Shuttle schedule. The Columbia accident suspended construction, and Russia kept the ISS alive until the Shuttle returned in 2005. Construction was slowed by the prudent flight rate and the ISS was completed this year. It is scheduled to be decommissioned in 2015, and splashed into the Pacific Ocean.

It is now acknowledged that such a course would shred the current International Partnership involving the ISS. Further, retirement of the Shuttle puts the ISS on fragile footing with regard to supply and maintenance.

The Commission entertained three scenarios:

  • Scenario 1: End U.S. Participation in the ISS at the end of 2015.
  • Scenario 2: Continue ISS Operations at the Present Level to 2020.
  • Scenario 3: Enrich the ISS Program and Extend through 2020.

Scenario 1 was rejected. Scenario 2 keeps the ISS alive for use by the international community, but does “not allow the ISS to achieve its full potential as a National Laboratory or as a technology testbed. The majority of the funding is devoted to sustaining basic operations and providing transportation”.

With Scenario 3, the Commission provides discussion and insight into the importance of additional funding associated with the extension of the ISS mission. Two quotes illustrate this:

The National Research Council Space Studies Board has recently initiated a decadal survey of life and microgravity science that will identify key scientific issues and strategies for addressing them. This is the first decadal survey in this area, and it will bring the most modern scientific understanding to bear on what questions may be answered in the decade through 2020

The Committee believes that the Space Station can be a valuable testbed for the life support, environmental, and advanced propulsion technologies, among others, that will be needed to send humans on missions farther into space. It also has the potential to help develop operational techniques important to exploration.

Having examined two active human space flight programs, the Committee waded into the thorny world of the Briar Patch.

4.3 The Constellation Program

The Constellation Program consists of the Orion crew exploration vehicle (CEV), the Ares I crew launch rocket, the Ares V cargo launch rocket and the Altair Lunar surface access module (LSAM).

The Orion was originally designed to field a crew of six for missions as long as six months, with a service module and launch abort system (LAS). Due to reduced capabilities anticipated for the Ares I, the Orion is facing continuing design changes, reducing its capacity to four crew, and requiring other design compromises. The report concludes that:

When compared to historical programs, the most likely delay to the Orion availability approaches 18 months. Additional critical paths exist through ground test and flight test.

At this point, the report examines the historical record and the mismatch between program contend and funding (see Figure 4.3.2-1. Constellation Program Funding Profiles. Source: NASA, p. 59):

  • ESAS original funding was scheduled to rise from $4.5 Billion in 2009 to $10.0 Billion in 2017.
  • Fiscal Year 2009 budget was to rise from $3.3 Billion to $8.3 Billion by 2017.
  • Fiscal Year 2010 budget rises from $2.9 Billion to $6.8 Billion in 2017.

These cuts have severely hampered the Constellation Program. This is a 45% reduction in budget in 2009 from the ESAS budget voted by Congress to the actual appropriated amount, and a 32% reduction by 2017. Congress and the previous administration are to blame for failing to fulfill their promises (what’s new?), and NASA is to blame for believing the unfunded promises of the politicians. Plenty of rope to hang everybody.

The next target of the Commission is the Ares V (about which much will be said later). To quote the report, “The Ares V, still in conceptual design, promises to be an extremely capable rocket—able to lift 160 metric tons of cargo into low-Earth orbit”. Now this classification of Ares V is interesting, because as we have previously noted, the Program of Record (PoR – Constellation; see CxP 70000 Constellation Architecture Requirements Document (CARD) Rev 3 Change 001, March 2009), requires that 71.1 mt of cargo be sent to the Moon (“the lander must mass no more than 45,000kg, Orion mass 20,185kg, ASE mass 890kg and there is 5,000kg of Manager’s Margin included for safety. That’s a grand total of 71,075kg or 71.1mT of total spacecraft mass being pushed thru TLI”). This is one of the “Misses” that the Commission makes. Instead of scoring proposed architectures by the requirements of the program proposed to justify the architecture, scoring seems to have been done against an architecture, absent the program. One wonders why Ares V needs to be so big.

Altair is by-passed in this chapter with a reference back to chapter 3.0. Subsequent to the release of the Commission’s report, development of Altair has been suspended, pending decisions by the current administration.

Finally, the Committee deals gingerly with Ares I:

The Ares I is currently dealing with technical problems of a character not remarkable in the design of a complex system – problems that should be resolvable with commensurate cost and schedule impacts. Its ultimate utility is diminished by schedule delays, which cause a mismatch with the programs it is intended to serve.

We are left, therefore, with hits and misses so far. Hits include the Goal. Also, the value of the Shuttle for up-mass and down-mass in the support of the ISS. Furthermore, the potential value of the ISS for scientific research, international cooperation, space based construction and maintenance, technological testing and human factor research.

Misses focus around the arbitrary choice of hardware capability without regard to Goal or mission.

Part 4 next.

(Part 1. Part 2. Part 3. Part 4. Part 5. Wrap Up.)

Posted in Asteroids, Augustine Commission, Comets, Direct, European Space Agency, Human Exploration, International Space Station, Moon, Mars and beyond, NASA, Space, Space Exploration | Tagged: , , , , , , , , , , , , | 5 Comments »

Ares 1-X

Posted by drdave on October 27, 2009

Ares 1-X is scheduled for launch this morning, and we are watching on NASA – TV. Currently, they are trying to remove the cover on the instrument probe on the top of the rocket. Delay until it comes loose.

The cord has finally separated. Ares 1-X is due for 9:44 AM EDT, assuming the weather holds. At 10 minutes before launch, the area is clear for launch.

Ares 1-X on Launch Pad

Ares 1-X on Launch Pad. Credit: NASA TV.

Removing Probe Cover

Removing the Probe Cover. Credit: NASA TV.

And now it is delayed by a ship in the area. The Air Force Range Safety team is having the ship turn around, and will clear the range soon.

Now we have a discussion of the weather window closing and they are trying to make up for the delay. Now poling launch team. Everyone is Go and they are getting a new launch time. Which is now 13:49 GMT (9:49 EDT).

T-4 minutes and counting. We got down to T-2:39 and they are resetting the clock due to launch weather officer stating weather would be no-go at T-0.

T Minus 2:39

T Minus 2:39. Credit: NASA TV.

Hold.  Waiting for Weather

Hold. Waiting for Weather. Credit: NASA TV.

T-0 is now scheduled for 10:54 AM EDT. Ares 1-X has been safed, and the count has been recycled to T-4 minutes and holding.

Hold for Weather

Hold for Weather. Credit: NASA TV.

Holding for Weather

Pad Winds – Holding at T minus 4 Minutes. Credit: NASA TV.

At 10:24 EDT we have about 30 minutes left in the hold. The latest problem is the wind speed at the pad is now above the 20 knot limit, which makes the launch “red”.

Currently at 10:36 EDT, the rocket is green, conditions are red and they expect to pick up the count in 15 minutes. Conditions are not looking promising. Kathy Winters, weather, states the open band expected 10:54 AM is narrowing. Other than weather, everything is currently green.

The Launch Director has announced 11:04 AM EDT as the new launch time.

Quote from Nasa:

The range is not available after noon today due to reasons such as airspace and warning areas, planes operating on flight plans, and other issues. Today’s launch window ends at noon.

The count is now scheduled to resume at T-4 minutes at 11:15 EDT with launch at 11:19 AM. There is a 25 minute weather window. After that, the weather will degrade.

The launch has now been moved up 5 minutes to 11:14 AM EDT. And then pushed back to 11:19 due to weather.

Weather reports green on all constraints with 2 minutes to resumption of the count.

Pad winds at 21 kts, and the launch gets bumped “a bit”. The Launch Director notes that if they miss the current resumption they will likely hang it up for the day.

The launch is scrubbed.

Posted in NASA, Rocket, Space | Tagged: , , | 1 Comment »

The Augustine Commission – Final Report – Hits and Misses – Part 2

Posted by drdave on October 26, 2009

(Part 1. Part 2. Part 3. Part 4. Part 5. Wrap Up.)

In Part 1, we looked at the pieces strewn about our living room floor. Let’s take a closer look at the Erector Set left behind by the Augustine Commission. The pieces parts are contained in Chapters 3-6.

Chapter 3.0 Goals and Future Destinations for Exploration

Most discussions concerning the Final Report have noted the importance of the having a Goal established in order to define both destinations and architectures to achieve them. Lets start with this extended quote from the Final Report:

3.1 Goals for Exploration

We explore to reach goals, not destinations. It is in the definition of our goals that decision-making for human spaceflight should begin. With goals established, questions about destinations, exploration strategies and transportation architectures can follow in a logical order. While there are certainly some aspects of the transportation system that are common to all exploration missions (e.g. crew access and heavy lift to low-Earth orbit), there is a danger of choosing destinations and architectures first. This runs the risk of getting stuck at a destination without a clear understanding of why it was chosen, which in turn can lead to uncertainty about when it is time to move on.

One can certainly agree with the rationale for starting with Goals. However, the final phrase leads one to pause. Does the expression “when it is time to move on” mean that we abandon destinations along the path toward our Goals? Rather, does it mean that we add what’s next to our collection of destinations when we have gained the required competence and experience from work on the most recent addition to our expanding list of destinations? We shall keep these questions in mind as we work through Chapter 3.

The Commission set “charting a path for human expansion into the solar system” as the Goal. The Commission sees the development of competitive commercial industries and important national capabilities as one reason for setting the Goal they did. It also cited the resulting scientific, technological, engineering and mathematical skills as another reason for choosing this Goal. Finally, the moment when we “first learn to live on another planet” will be a milestone in human history.

3.2 Overview of Destinations and Approach

Destinations can be classified by duration of the mission: the Moon is days away, the Lagrange points weeks, the near-Earth objects months, a Mars fly-by a year, and a Mars landing is the longest—about 900 days for a round trip using the most likely approach. The result of two cycles of analyses collapsed the destinations and associated missions into three candidates:

  • Mars First. It is widely accepted that Mars represents the most likely candidate for a permanent expansion of human civilization beyond the Earth. Mars is unquestionably the most complex environment for exploration, and fits Dr. Steve Squyres criteria for deploying human investigators.
  • Moon First. Missions to the Moon would enable the development of the operational skills and technology for landing on, launching from and working on a planetary surface.
  • Flexible Path. The Commission notes that the Flexible Path option means “we must learn to operate in free space for hundreds of days, beyond the protective radiation belts of the Earth, before we can confidently commit to exploring Mars”.

The Final Report then examines each of these options.

3.3 Mars First

The possible scenarios for Mars First are two, described by the Commission this way:

Two scenarios have been developed to examine the human exploration of Mars. In the first, the surface of Mars would be the initial and only destination, and all resources would be focused on reaching it as soon as possible. In the second, systems would be designed for Mars missions, but would be first verified on several test flights to the Moon. The latter would require some hardware modification, but would test the systems at a planetary body near the Earth before committing to a multi-year mission to Mars. In the end, the Committee decided to use the variant with a brief test flight program of equipment and procedures on the Moon as the reference Mars First option.

The first scenario was analyzed based on the existing 2007 NASA Human Exploration of Mars Design Reference Architecture 5.0 (NASA-SP-2009-566 and NASA-SP-2009-566-ADD). This architecture is shown in Figure 3.3.2-1 (p. 36). Figure 3.3.2-2 shows the architecture of first conducting several missions to the Moon.

The Commission concluded that the technological problems were many, and that a decade of research was required before design work could commence. Further, the costs were significantly higher than for either of the other two options.

Clearly, either of the possible scenarios leaves little or no infrastructure in place, and fails the Goals criteria.

3.4 Moon First

The Commission next examined the Moon First. Here, the possibility of resource utilization for supplying propellant to the space around the Earth-Moon system, as well as the scientific value of exploration based on our incomplete understanding of the Moon drive two possible scenarios. The first is a Lunar Base, where a permanent station is established, most likely at the South Pole where solar energy would be available at all times. The emphasis would be on local exploration and resource utilization for propellant manufacture.

The alternate scenario was Lunar Global, where missions of from 14 to 180 days would be flown to a variety of sites, adjusting the program as discoveries were made.

Either of these programs would be supported by one of three architectures considered by the Committee:

  • Constellation “1.5 launch” architecture – one Ares I with Orion, plus one Ares V with the Altair lander. This combination is Integrated Option 3 in Chapter 6.
  • Ares V Lite “dual” architecture – two Ares V Lites, one with the Orion, and one with the Altair lander. This combination is Integrated Option 4A in Chapter 6.
  • A more directly Shuttle-derived launcher, which requires three launches for a crew mission plus one commercial launch of crew to low-Earth orbit. This combination is Integrated Option 4B in Chapter 6.

One is immediately struck by two contradictions within these architectures. First is the requirement for three launches for the more directly Shuttle-derived launcher, when two launches of the Jupiter 246 exceed the Constellation Program requirements. See this data sheet for the Jupiter 130 Crew and Cargo (60 mt to low earth orbit) and data sheet for the Jupiter 246 Crew and Cargo launcher (96 mt to LEO and 79 mt through TLI).

The second more serious contradiction is allowing Ares V Lite to launch crew, but requiring the Shuttle-derived vehicle to only carry cargo. The problem we face is that Ares V Lite has:

  • New Engines
  • New External Tank (10 meters)
  • New Solid Rocket Boosters (5 segment)

Each of these requires independent rating for human flight. On the other hand, both the side-mount Shuttle-derived launch vehicle and the in-line Shuttle-derived vehicle have:

  • Existing SSME (Space Shuttle Main Engines)
  • Existing External Tank (8.4 meters)
  • Existing 4 segment Solid Rocket Boosters (SRB)

The SSMEs and the 4 segment SRBs are already human flight qualified. The modifications to the ET would require flight testing for qualification of the in-line vehicle, but are minor compare to designing and building a brand new 10 meter tank. While the side-mount Shuttle-derived launch vehicle has disadvantages for launching crew, the in-line Shuttle-derived vehicle has no such drawbacks.

These contradictions place unwarranted obstacles on the Shuttle-derived vehicles, especially the in-line version.

3.5 The Flexible Path to Mars

The Commission states:

“The goal is to take steps toward Mars, learning to live and work in free space and near planets, under the conditions humans will meet on
the way to Mars. We must learn to operate in free space for hundreds of days, beyond the protective radiation belts of the Earth, before we can confidently commit to exploring Mars.

The primary attraction of this option is that we can build increasing confidence, infrastructure and expertise as we move from one destination to the next.

There are multiple destinations. Each one offers the opportunity to build different skills. Especially valuable would be for international partners to take on the challenge of Lunar Surface Exploration while NASA continues the research and development required for the Flexible Path missions. Both commercial enterprises and International Partners could handle the propellant delivery to the depots in LEO, EML-2, and eventually Phobos. All of this is aimed at the eventual establishment of permanent human presence on Mars.

From the perspective of the Goals given by the Commission, the Flexible Path option is the strongest.

3.6 Summary of Strategies for Exploration Beyond Low-Earth Orbit

The Committee concludes as follows:

Mars is the ultimate destination for human exploration of the inner solar system; but it is not the best first destination. Both visiting the Moon First and following the Flexible Path are viable exploration strategies. The two are not necessarily mutually exclusive; before traveling to Mars, we might be well served to both extend our presence in free space and gain experience working on the lunar surface.

In the next post, we will look at the existing human space flight programs discussed in Chapter 4.0.

(Part 1. Part 2. Part 3. Part 4. Part 5. Wrap Up.)

Posted in Asteroids, Astronauts, Augustine Commission, Comets, Direct, Human Exploration, International Space Station, Moon, Mars and beyond, NASA, Space, Space Exploration, Space Settlement | Tagged: , , , , , , , , , , , , , , , , , , , , | 6 Comments »

The Augustine Commission – Final Report – Hits and Misses – Part 1

Posted by drdave on October 23, 2009

(Part 1. Part 2. Part 3. Part 4. Part 5. Wrap Up.)

The final report from the Augustine Commission is out. And while the report suffers from the 90 day time constraint, what it does do is open the discussion of what we are doing in space. The answer the Commission gives is to “Expand Human Civilization into the Solar System”. Having given that answer, however, the report then goes back to its origins and begins its “Review of U.S. Human Space Flight Plans”.

Starting Points

Following some initial public meetings, the Committee decided that it should answer the following questions:

  • 1. What should be the future of the Space Shuttle?
  • 2. What should be the future of the International Space Station (ISS)?
  • 3. On what should the next heavy-lift launch vehicle be based?
  • 4. How should crews be carried to low-Earth orbit?
  • 5. What is the most practicable strategy for exploration beyond low-Earth orbit?

The report then details how the Commission arrived at the potential programs that were evaluated. Starting with a matrix of over 3,000 possible combinations of destinations, hardware and missions based on the five questions, the Committee developed five options, which were explored and evaluated. Several of them had alternatives. The options are:

  • Option 1. Program of Record as Assessed by the Committee, Constrained to the FY 2010 budget, providing funds for the Shuttle into FY 2011 and including sufficient funds to deorbit the ISS in 2016.
  • Option 2. ISS and Lunar Exploration, Constrained to FY 2010 Budget. It extends the ISS to 2020, and begins a program of lunar exploration using a derivative of Ares V, referred to here as the Ares V Lite.
  • Option 3. Baseline Case—Implementable Program of Record. This is an executable version of the Program of Record. Budgeting for the completion of remaining flights on the Shuttle manifest in 2011 and including additional funds for the de-orbit of the ISS.
  • Option 4. Moon First. It consists of the content and sequence of that program–de-orbiting the ISS in 2016, developing Orion, Ares I and Ares V, and beginning exploration of the Moon using the Altair lander and lunar surface systems
  • Variant 4A is the Ares V Lite variant. This option retires the Shuttle in FY 2011 and develops the Ares V Lite heavy-lift launcher for lunar xploration.
  • Variant 4B is the Shuttle extension variant. It offers the only foreseeable way to eliminate the gap in U.S. human-launch capability: by extending
    the Shuttle to 2015 at a minimum safe-flight rate.
  • Option 5. Flexible Path. It operates the Shuttle into FY 2011, extends the ISS until 2020. The destinations include Near Earth Objects, the Lagrange points around the Earth-Moon system and the moons of Mars.
  • Variant 5A is the Ares V Lite variant. It develops the Ares V Lite, the most capable of the heavy-lift vehicles in this option.
  • Variant 5B employs an EELV-heritage commercial heavy-lift launcher and assumes a different (and significantly reduced) role for NASA. It has an advantage of potentially lower operational costs, but requires significant restructuring of NASA.
  • Variant 5C uses a Shuttle-derived, heavy-lift vehicle, taking maximum advantage of existing infrastructure, facilities and production capabilities.

It is at this point that Chapter 1.0 Summary ends.

Interlude

Chapter 2.0 U.S. Human Spaceflight: Historical Review offers a brief four page summary of the past 50 years.

Boring Details

Having laid out the summary questions and options, the report then elaborates with detailed work as follows:

  • Chapter 3.0 Goals and Future Destinations for Exploration
  • Chapter 4.0 Current Human Spaceflight Programs
  • Chapter 5.0 Launch to Low-Earth Orbit and Beyond
  • Chapter 6.0 Program Options and Evaluation

These are interesting chapters with lots of studies, trades, costs, schedules and contradictions destined to engage the various factions concerned with human space flight for a long time. We will return here in future posts to engage some of these arcane turf wars.

Problems Requiring Solutions

In the mean time, Chapter 7.0 Critical Technologies for Sustainable Exploration, has the significant factors required to eventually come to grips with a real vision for space exploration.

7.1 Fundamental Unknowns lists these three key problems:

  • (1) the effects of prolonged exposure to solar and galactic cosmic rays on the human body
  • (2) the impact on humans of prolonged periods of weightlessness followed by a sudden need to function, without assistance, in a relatively strong gravitational field
  • (3) the psychological effects on individuals facing demanding tasks in extreme isolation for well over year with no possibility for direct outside human intervention.

7.2 Propellant Storage and Transfer in Space discusses the advantages of refueling rockets in space. The traditional mission involves launching your Moon rocket and payload and all the propellant needed to leave Earth orbit and land on the Moon. Not a lot of cargo gets landed on the Moon because most of the payload is propellant.

However, if you launch your Moon rocket and it arrives empty at the propellant depot, you can add propellant. Since you don’t have propellant in the rocket, the mass of the rocket and cargo constitutes the entire payload. This means a lot more cargo gets to the Moon.

7.3 In Situ Propellant Production and Transport involves using the resources from objects in the Solar System to produce propellant. These bodies include the Moon, Mars, asteroids and comets.

7.4 Mars Orbit to Surface Transportation. Quoting from the report:

“The entry, descent and landing of cargo on Mars is difficult because Mars has sufficient atmosphere to drive the design of landing systems, but inadequate atmosphere for feasible parachutes or wings to safely land astronauts on the surface. Scientific probes landing on Mars have used a complex mix of aerodynamic braking and rocket propulsion. These techniques will have to be improved before larger robotic or crewed missions can be sent to Mars. This research and technology development program needs to be started soon, because it will require many iterations and increasingly larger missions before NASA is ready to demonstrate a safe, crewed Mars landing. Meanwhile, the intermediate results would greatly benefit future robotic missions.”

7.5 Advanced Space Propulsion include solar and nuclear powered systems.

7.6 Technology Summary provides two charts covering a large number of items:

  • Figure 7.6-1. Technology opportunities to impact near- and mid-term exploration capabilities and sustainability.
  • Figure 7.6-2. Technology opportunities impact longer-term capabilities and sustainability.

International Partners

Chapter 8.0 Partnerships covers the advantages and problems associated with partnerships, both International and intra-governmental, such as Department of Defense and national security interests.

What Are We To Do

The final report of the Augustine Commission ends with a series of concluding remarks and recommendations about costs, goals and management.

And we are left with the sense that something is missing.

We have a lot of pieces spread out on the floor in front of us. There are snippets of vision laying here and there. What are we to do with it all?

Let us try and bring about some order:

  • What gets decided in the next 6 months is likely to affect the next hundred years of exploration.
  • We have a lot of technological problems to solve, so we are not going to go as fast as everybody wants to go.
  • Building in small steps and becoming good at each step means we can develop a robust infrastructure. Building the International Space Stations has taught us a lot of lessons about how to do things in space, as well as how not to do things.
  • It will take more wealth than the American taxpayer can afford. The tasks require a concerted continuation by the rest of the nations in the efforts already underway.
  • A sustained and sustainable program will have to learn to live off the land. The less we have to bring with us, the less we have to bring with us (getting mass up out of the Earth’s gravity well is very expensive).

The worst thing would be to make a mad dash to Mars, send pictures back of astronauts saluting the flag, and leaving nothing behind (except footprints).

No propellant depots, no interplanetary space tugs, no scientific observatories, no resource utilization, no jobs, no economic engine.

There is no guarantee that the rest of the Solar System actually has a future with human civilization expanding through it. If such a future exists, we will have to build it carefully.

(Part 1. Part 2. Part 3. Part 4. Part 5. Wrap Up.)

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The Augustine Commission – Final Report

Posted by drdave on October 22, 2009

The final report of the Augustine Commission (all 155 pages) can be obtained here. The press conference re-iterated the Summary Report. Now we can digest the report and see what happens.

Table of Contents
Preface 7
Executive Summary 9
Chapter 1.0 Introduction 19
Chapter 2.0 US Human Spaceflight: Historical Review 27
Chapter 3.0 Goals and Future Destinations for Exploration 33
3.1 Goals for Exploration 33
3.2 Overview of Destinations and Approach 33
3.3 Mars First 35
3.4 Moon First 37
3.5 The Flexible Path to Mars 40
3.6 Summary of Strategies for Exploration Beyond Low-Earth Orbit 43
Chapter 4.0 Current Human Spaceflight Programs 47
4.1 The Space Shuttle 47
4.2 The International Space Station 51
4.3 The Constellation Program 57
Chapter 5.0 Launch to Low-Earth Orbit and Beyond 63
5.1 Evaluation Methodology for Launch Vehicles 63
5.2 Heavy Lift to Low-Earth Orbit and Beyond 64
5.3 Crew Launch to Low-Earth Orbit 68
5.4 Additional Issues in Launcher Selection 72
Chapter 6.0 Program Options and Evaluation 77
6.1 Evaluation Criteria 77
6.2 Key Decisions and Integrated Options 79
6.3 Integrated Options Constrained to the FY 2010 Budget 84
6.4 Moon First Integrated Options Fit to the Less-Constrained Budget 85
6.5 Flexible Path Integrated Options Fit to the Less-Constrained Budget 91
6.6 Comparisons Across Integrated Options 94
Chapter 7.0 Critical Technologies for Sustainable Exploration 99
7.1 Fundamental Unknowns 99
7.2 Propellant Storage and Transfer in Space 100
7.3 In Situ Propellant Production and Transport 101
7.4 Mars Orbit to Surface Transportation 102
7.5 Advanced Space Propulsion 102
7.6 Technology Summary 103
Chapter 8.0 Partnerships 105
8.1 International Partnerships 105
8.2 US Intra-Government Partnerships 107
Chapter 9.0 Concluding Observations 111
9.1 Establishing Goals 111
9.2 Matching Resources and Goals 111
9.3 NASA Management Challenges 112
9.4 Systems Engineering 113
9.5 Procuring Systems 113
9.6 Managing the Balance of Human and Robotic Spaceflight 114
9.7 Concluding Summary 115
Appendices
A Committee Member Biographies 117
B Committee Staff 123
C Review of US Human Space Flight Plans Statement of Task 127
D Charter of the Review of US Human Space Flight Plans Committee 131
E List of Full Committee Meetings and Locations 135
F Briefers and Committee Contacts 137
G Communications and Public Engagement 141
H Bibliography 145
Glossary Acronyms and Abbreviations 153

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The Augustine Commission – Final Report and Press Conference

Posted by drdave on October 21, 2009

Tune in to NASA TV for the Press Conference and the release of the Final Report on Thursday, 22 October 2009, at 10:00 AM Phoenix time.

Press Conference – Washington, D.C.
10.22.09

Date and Time: October 22, 2009 – 1 pm EDT
Location Information:
Zenger Room of the National Press Club
529 14th St. NW, in Washington, D.C.

The Review of U.S. Human Space Flight Plans Committee
Chairman Norman Augustine will hold a press conference at 1 p.m. EDT,
on Thursday, Oct. 22, in the Zenger Room of the National Press Club, 529 14th St. NW, in Washington.

Augustine will be accompanied by committee member Ed Crawley. Printed copies of the committee’s
final report will be available during the press conference and an electronic copy of the report
will be posted to the committee’s Web site at the start of the briefing.

The press conference will be broadcast on NASA Television’s Media Channel
and streamed on the agency’s Web site.

NSS Phoenix summary posts on the Final Report:

(Part 1. Part 2. Part 3. Part 4.)

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