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NASA – The Rumor Mill

Posted by drdave on December 18, 2009

Following on the Tuesday meeting at NASA headquarters concerning revamping the governance structure, and Wednesday’s meeting between NASA administrator Charles Bolden and President Barack Obama, the rumor mill has been if full fury.

Wayne Hale offered this tweet: “Wondering if reports on Obama-Bolden meeting are accurate or just blather. No hard news has appeared.” To which Bob Jacobs, NASA’s deputy assistant administrator of Public Affairs responded: “Inaccurate. The meeting was informational, not decisional…”. Of course, that’s NASA’s spokesperson. Amy Klamper at Spacenews.com thinks “New Direction for NASA Could Wait Until February.”

Now comes Science magazine’s (AAAS) Insider report concerning the outcome of the meeting:

President Barack Obama will ask Congress next year to fund a new heavy-lift launcher to take humans to the moon, asteroids, and the moons of Mars, ScienceInsider has learned. The president chose the new direction for the U.S. human space flight program Wednesday at a White House meeting with NASA Administrator Charles Bolden, according to officials familiar with the discussion. NASA would receive an additional $1 billion in 2011 both to get the new launcher on track and to bolster the agency’s fleet of robotic Earth-monitoring spacecraft.

The major elements include:

  • Elimination of the Ares I rocket
  • Recommend Commercial development of Low Earth Orbit (LEO) launch capability for cargo and then crew.
  • Development of a smaller heavy lift rocket along the lines proposed by the old NLS (National Launch System) NASA investigated in the early 1990’s and revived by the Direct Team between 2005 and today.
  • Addition of $1 Billion to the Budget for NASA
  • European countries, Japan, and Canada would be asked to work on a lunar lander and modules for a moon base.
  • Focus on being able to perform a variety of missions including Near Earth Objects, Lagrange points, the Moon, the moons of Mars (Phobos and Deimos). See Option “5D”
  • Additional probes to the Moon, Mars and and the moons of Mars.

Immediate blow back is expected from Senator Richard Shelby, who has asked the Inspector General at NASA to investigate “corruption” within the Augustine Commission. Shelby stated that several Augustine panel members were registered lobbyists who took “direct advantage of their temporary roles on the Commission to further their personal business.” This has been interpreted as a shot across the bow in the fight over Ares I and the jobs it creates at the Marshall Space Flight Center in Shelby’s state of Alabama. Whose bow it was aimed at is in question, and it looks like an act of desperation.

However, as noted in our Wrap Up report on the Augustine Commission, time is of the essence with regard to jobs and the retention of skills associated with building the 8.4 meter External Tank used by the space shuttle and the proposed heavy launch vehicle derived from the shuttle. If the politicians resist the change that’s coming to NASA, they may lose everything.

Denials to the Science Insider article came immediately from NASA and the White House. NASA spokesman Morrie Goodman said the article was “speculation.” White House spokesman Nicholas Shapiro echoed that characterization.

Posted in Astronauts, Augustine Commission, Commercial Spaceflight, Direct, European Space Agency, Human Exploration, International Space Station, Moon, Mars and beyond, NASA, Robotic Exploration, Space, Space Exploration | Tagged: , , , , , , , , , , , , , , , , , , | Leave a Comment »

The Augustine Commission – Final Report – Hits and Misses – Part 5

Posted by drdave on November 22, 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. And in Part 3, the three current Human Space Flight programs were reviewed (International Space Station, the Space Shuttle and the Constellation Program). In Part 4, we looked at the launch vehicles examined by The Augustine Commission.

Chapter 6 of the Augustine Commission Final Report deals with Program Options and Evaluation. This is one of the many contentious issues commentators have with the Commission. While they did select five possible exploration programs (Chapter 6), and while they did evaluate various launch vehicles (Chapter 5), the Committee seems to have ignored the possibility that different launch vehicles have greater or lesser ability to cover the five exploration programs. This failure may in the end, prove to be disastrous for human space exploration. As we write, the Space Shuttle infrastructure is being actively dismantled. The end result of failing to evaluate the physical infrastructure and the human infrastructure capable of supporting a Shuttle derived architecture may be that the United States is left with no heavy lift human space flight capability for at least the next several decades. We may have surrendered our space faring capability to Europe, China, Russia, India and Japan.

6.1 Evaluation Criteria

As noted by the Commission:

The Committee did not intend that the evaluation would generate a single numerical score; rather, it would provide a basis for comparison across options, highlighting the opportunities and challenges associated with each. Assigning weights to individual figures of merit is within the purview of the ultimate decision-makers.

Three primary evaluation dimensions were identified:

  • Benefits to Stakeholders
  • Risk
  • Budget Realities

These three dimensions were expanded into 12 criteria for comparing the options.

  • Exploration Preparation
  • Technology Innovation
  • Science Knowledge
  • Expanding and Protecting Human Civilization
  • Economic Expansion
  • Global Partnerships
  • Public Engagement
  • Schedule and Programmatic Risk
  • Mission Safety Challenges
  • Workforce Impact
  • Programmatic Sustainability
  • Life-Cycle Cost

6.2 Key Decisions and Integrated Options

6.2.1 Key Decisions

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?

6.2.2 Integrated Options

The Committee identified five basic options: One based on the Program of Record (POR – Constellation – Ares I and V, Orion and Altair), and four alternatives. Options 2 and 3 were budget compatable alternatives to the POR. Option 4 was a Moon First program (with two variations), and Option 5 was the Flexible Path (avoiding the gravity well of the Moon).

6.2.3 Methodology for Analyzing the Integrated Options

Two budgets were used. The “Constrained Budget” used the FY 2010 budget, while the “Less Constrained Budget” allowed for an increase by 2014 of $3 Billion per year higher than FY 2010.

6.2.4 Reference Cases of the Entirely Unconstrained Program of Record

The Program of Record was evaluated and found to be a total of $45 Billion over the FY 2010 budget by 2020, wherein it is $5 Billion a year over FY 2010 in 2016 and $7 Billion per year over FY 2010 in 2019.

6.3 Integrated Options Constrained to the FY 2010 Budget

6.3.1 Evaluation of Integrated Options 1 and 2

Option 1 was found to allow for rocket development, but lacked funds for exploration. Option 2 extends the lifetime of the ISS, delays rocket development, and has no funds for exploration.

6.3.2 Examination of alternate budget guidance

The Committee found no alternatives to Options 1 or 2 that were viable under the FY 2010 budget. This conclusion has been disputed.

6.4 Moon First Integrated Options Fit to the Less-Constrained Budget

6.4.1 Evaluation of Integrated Options 3 and 4

Option 3 was to execute the POR under a less constrained budget. The ISS is de-orbited in 2010, and the Shuttle flies the remaining missions into 2011. Human lunar return occurs in the mid 2020s and the lunar base becomes operation late in the decade. An alternate extending ISS to 2020 was found to push these dates out by three to four more years.

Option 4 uses the less constrained budget, scraps Ares I and substitutes commercial crew services by 2016 It extends the ISS to 2020. Ares V is scrapped in favor of a dual-launch Ares V Lite vehicle for lunar missions.

Option 4A retires the Shuttle in 2011, while Option 4B extends the Shuttle to 2015 and develops a Shuttle Derived Heavy Lift vehicle in place of Ares V Lite.

6.4.2 Examination of the key decision on the ISS extension

Given the International Partnerships that have been developed, and the fact that the extension to 2020 would only delay the lunar return by a few years, the Committee found that the extension provides greater value than ending the ISS mission.

6.4.3 Examination of the key decision on Ares V vs. Ares V Lite dual launch

Baseline Ares V has more launch capability than the Saturn V, but current NASA studies show that when used in combination with Ares I, it does not have enough launch capability to robustly deliver the currently planned landing and surface systems to the Moon.

The Committee concluded that Ares V Lite represents less development risk, likely will reduce costs and provides more substantial margin for the lunar mission.

6.4.4 Examination of the key decision on the provision of crew transport to low-Earth orbit

Commercial crew services, based on a high-reliability rocket with a capsule and launch escape system could significantly reduce development costs, as well as lower operating costs.

6.4.5 Examination of the key question on Shuttle extension

The Committee favored early retirement of the Shuttle (2010 or 2011), although they noted several advantages to Shuttle extension to 2015, including up-mass and down-mass capability and workforce retention.

6.5 Flexible Path Integrated Options Fit to the Less-Constrained Budget

6.5.1 Evaluation of Integrated Option 5

Option 5 operates the Shuttle into 2011 and extends the International Space Station mission until 2020. A variety of destinations beyond low earth orbit are possible. The Committee developed three variants of this option.

  • Option 5A develops the Ares V Lite, visits the Lagrange points, near Earth objects, on-orbit refueling and achieves a lunar return by the end of the 2020s.
  • Option 5B develops commercial heavy lift capability, restructures NASA, and follows a similar mission profile as 5A, but on a slower time line.
  • Option 5C scraps Ares V Lite and develops a Shuttle Derived Heavy Lift vehicle. 5C follows a similar mission profile as 5A, but on a slower time line.

6.5.2 Examination of the key question on Ares V family vs. Shuttle-derived heavy launcher

While the Shuttle derived in-line launch vehicle (SDLV) with two four-segment solid rocket motors (SRM) and the 8.4 meter external tank (ET) was the 2005 ESAS candidate for the cargo vehicle, it was forced to evolve into the Ares V due to the problems encountered with the underpowered Ares I. For some reason, the Committee decided that in order to match the capabilities of the Ares V, or the Ares V Lite dual-launch mission, that there had to be three SDLV launches. Therefore, operations would be more costly.

This is a clear Committee miss, as the current planned lunar return missions can be accomplished with good margin by a dual-launch SDLV program, thus costing less than the Ares V Lite. There is no need for the enhanced capabilities of the dual-launch Ares V Lite.

6.5.3 Examination of the key question on NASA heritage vs. EELV-heritage super-heavy vehicles

The Committee considers the EELV-heritage super-heavy vehicle to be a way to significantly reduce the operating cost of the heavy lifter to NASA in the long run. It would be a less-capable vehicle, but probably sufficiently capable for the mission. Reaping the long-term cost benefits would require substantial disruption in NASA, and force the agency to adopt a new way of doing business.

6.6 Comparisons Across Integrated Options

6.6.1 Cross-option comparisons

The Flexible Path program (Option 5A) scores more highly than the Baseline (Option 3) on 9 of the 12 criteria outlined in section 6.1 ( See figure 6.6.1-1). The higher rankings include:

  • Exploration Preparation (due to much more capable launch system)
  • Technology (due to investment in technology)
  • Science (because of more places visited)
  • Human Civilization (due to the ISS extension)
  • Economic Expansion (because of commercial involvement in space elements and crew transport)
  • Global Partnerships (gained by extending the ISS)
  • Public Engagement (by visiting more new locations, and doing so each year)
  • Schedule (exploring beyond low-Earth orbit sooner)
  • Life-Cycle Costs (due to commercial crew services)

6.6.2 Examination of the key question on exploration strategy

Three exploration strategies were examined in Chapter 3. The choice of Mars First was found not to be viable due to technological problems. Two strategies remained:

  • Moon First on the Way to Mars, with surface exploration focused on developing capability for Mars.
  • Flexible Path to Mars via the inner solar system objects and locations, with no immediate plan for surface exploration, then followed by exploration of the lunar and/or Martian surface.

The Moon first is favorable to lunar science and exploration (although much can be done robotically). The Flexible Path missions explore more of the Solar System, while initially doing less on the Moon. Flexible Path has the advantage of developing infrastructure for deep space exploration, including the moons of Mars and Mars itself. The Committe notes that:

Considering that we have visited and obtained samples from the Moon, but not near-Earth objects or Mars, and also that the Flexible Path develops the ability to service space observatories, the Science Knowledge criterion slightly favors the Flexible Path. Broadly, the more complex the environment, the more astronaut explorers are favored over robotic exploration. In practice, this means that astronauts will offer their greatest value-added in the exploration of the surface of Mars.

Final Scoring

Although the Augustine Commission did not publish a final tally of the scores (for reasons they made clear), the following table does compare and tabulate the scores.

Option Description Science Safety Cost Schedule NASA / Industry Jobs US Skills Retention Exploration Capability Technology Space Colony Potential Commercial Benefit Public Engagement international Cooperation Sustainability Total
1 The Status Quo 0 0 0 -2 -1 -1 -2 -2 -2 -1 -1 -2 -1 -15
2 ISS Extension plus Moon 0 0 1 -2 -1 -1 -2 1 -1 1 -1 0 0 -5
3 Status quo + $3 B 1 -1 0 0 0 -1 0 0 0 0 0 -2 0 -3
4 Shuttle + Moon 1 -1 1 0 0 -1 1 1 1 1 0 0 0 4
4B Shuttle 2015 + Moon 1 -1 0 0 0 0 1 1 1 1 0 0 1 5
5A Flexible Path + Ares Lite 2 -1 1 1 0 -1 2 1 1 2 1 0 0 9
5B Flexible Path + Commercial 2 -2 2 1 0 -1 1 2 1 2 1 0 -1 8
5C Flexible Path + Jupiter 241 2 -2 0 1 0 -1 1 1 1 2 1 0 1 7

Option 5D: We will have more to say about this proposal in our final segment: “Wrapped Up” or “The Augustine Commission for Dummies”.

Option Description Science Safety Cost Schedule NASA / Industry Jobs US Skills Retention Exploration Capability Technology Space Colony Potential Commercial Benefit Public Engagement international Cooperation Sustainability Total
5D Flexible Path + Direct 2 -2 1 1 1 1 2 1 1 2 1 1 1 13

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

Posted in Asteroids, Astronauts, Augustine Commission, Comets, Commercial Spaceflight, Direct, Human Exploration, International Space Station, Moon, Mars and beyond, NASA, Robotic Exploration, Rocket, Satellites, Space, Space Exploration, Space Settlement, Technology | Tagged: , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , | 5 Comments »

JWST – James Webb Space Telescope

Posted by drdave on November 12, 2009

James Webb Space TelescopeCredit: NASA Video

The James Webb Space Telescope (JWST) is an infrared observatory, and a partial successor to the Hubble Space Telescope. JWST does not view visible light because light from the earliest universe has shifted toward the infrared (red shift).

Infrared sensitivity is required in order to see further back in time toward the beginning of the universe than either Hubble or ground based observatories.The James Webb Space Telescope is a joint venture between NASA, the European Space Agency (ESA) and the Canadian Space Agency (CSA). In all, fifteen countries are making contributions to JWST.

The are four main components to the scientific mission:

  • Search for the first stars and galaxies that formed after the Big Bang
  • Study galaxies and their formation and evolution
  • Understand the formation of stars and planetary systems
  • Study the origins of life on planetary systems

JWST is scheduled for launch in 2014 aboard an Ariane 5 rocket. It will take up residence at the Sun-Earth Lagrange point 2 (SEL-2). SEL-2 is 1,500,000 km beyond the Earth from the Sun (the Earth-Moon L2 is 61,500 km beyond the Moon). The location was chosen in order to be able to shield the telescope from the infrared radiation of the Sun and the Earth.

Currently, SEL-2 is occupied by the Wilkinson Microwave Anisotropy Probe (WMAP), which was launched 30 June 2001, and the Herschel and Planck observatories, which were launched together on an Ariane 5 on 14 May 2009.

The image at left is a cutaway diagram the the Ariane 5 rocket, illustrating how the JWST will fold up inside the payload fairing. With the large screen behind it, the JWST will be about 21 m in width. It will stand about three stories high. The main telescope mirror, which measures 6.5 m in diameter, is too large to launch in one piece. Instead, it consists of 17 individual mirror segments mounted on a frame which will be folded inside the fairing of the Ariane 5 at launch.

Once it arrives at SEL-2, it will unfold, as this animation shows.

There are four instruments designed to conduct the investigations on board the James Webb Space Telescope:

  • Mid-Infrared Instrument, or MIRI – provided by the European Consortium with the European Space Agency (ESA), and by the NASA Jet Propulsion Laboratory (JPL)
  • Near-Infrared Camera, or NIRCam – provided by the University of Arizona
  • Near-Infrared Spectrograph, or NIRSpec – provided by ESA, with components provided by NASA/GSFC.
  • Fine Guidance Sensor, or FGS – provided by the Canadian Space Agency. The FGS contains a dedicated Guider and a Tunable Filter Camera.
Cutaway: JWST inside Ariane 5

Credit: European Space Agency

Four InstrumentsCredit: NASA

 

Location

Credit: NASA

The image at left shows the locations of the four instruments in the Integrated Science Instrument Module (ISIM). Below, the image shows the location of the instrument package within the JWST.

The Mid-Infrared Instrument (MIRI) is an imager/spectrograph that covers the wavelength range of 5 to 27 micrometers. The camera provides wide-field broadband imagery, and the spectrograph module provides medium-resolution spectroscopy over a smaller field of view compared to the imager. The nominal operating temperature for the MIRI is 7K. Additional information can be found at the MIRI website, Space Telescope Science Institute.

The Near Infrared Camera (NIRCam) is an imager with a large field of view and high angular resolution. The NIRCam covers a wavelength range of 0.6 to 5 micrometers. More on NIRCam.

The Near Infrared Spectrograph (NIRSpec) measures the simultaneous spectra of more than 100 objects in a 9-square-arcminute field of view. This instrument provides medium-resolution spectroscopy over a wavelength range of 1 to 5 micrometers and lower-resolution spectroscopy from 0.6 to 5 micrometers. See the Space Telescope Science Institute information on NIRSpec.

The Fine Guidance Sensor (FGS) sensor is used for both “guide star” acquisition and fine pointing. See information from the Space Telescope Science Institute about NIRSpec.

Recent Events

In October, the NIRSpec Engineering Test Unit (ETU) was completed by Astrium, and will be shipped to the United States later this year for integration testing. For additional information on the ETU, see this article in Space News. Integration testing will allow work to continue while the final NIRSpec instrument is developed. Along with the NIRSpec ETU, a test model of the other European instrument, the Mid-Infrared Instrument (MIRI) will also be delivered.

See also:

The Wikipedia article on JWST.
NASA home page for JWST.
ESA home page for JWST.
CSA home page for JWST.
Make your own Paper Model of the JWST.
YouTube and JWST.

Posted in Astronomy, European Space Agency, Eye Candy, NASA, Robotic Exploration, Rocket, Satellites, Space | Tagged: , , , , , , , , | 2 Comments »

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.

Posted in Commercial Spaceflight, Robotic Exploration, Rocket, 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 »

Rosetta – Final Fly-By

Posted by drdave on October 20, 2009

Rosetta

Credit: ESA Image

The European Space Agency (ESA) spacecraft Rosetta will make its third and final flyby of the Earth a month from now. Rosetta will swing by Earth on 13 November and begin the final leg of its 10-year journey to the outer Solar System. Several observations of the Earth–Moon system are planned before the spacecraft heads out to study comet 67/P Churyumov-Gerasimenko.
A summary of the mission from ESA reads:

The International Rosetta Mission was approved in November 1993 by ESA’s Science Programme Committee as the Planetary Cornerstone Mission in ESA’s long-term space science programme. The mission goal was initially set for a rendezvous with comet 46 P/Wirtanen. After postponement of the initial launch a new target was set: Comet 67 P/Churyumov- Gerasimenko. On its 10 year journey to the comet, the spacecraft will pass by two asteroids: 2867 Steins (in 2008) and 21 Lutetia (in 2010).

The ESA Rosetta blog has been reactivated. The latest entry is here.

Steins

Credit: ESA Image of Approach to Steins

History

  • February 2004, Rosetta was launched by an Ariane-5 launch from Kourou in French Guiana.
  • March 2005, Rosetta makes its first fly-by of Earth, and heads toward Mars.
  • February 2007, Rosetta makes its fly-by of Mars
  • November 2007, Rosetta makes its second fly-by of Earth, and heads toward the asteroid belt.
  • September 2008, the Rosetta spacecraft encounters asteroid (2867) Steins.
  • November 2009, third Earth fly-by.
  • July 2010, Rosetta will encounter asteroid 21 Lutetia.
  • May 2011 – January 2014, Rosetta goes into hibernation on the way to comet 67 P/Churyumov- Gerasimenko.
  • May 2014, Rosetta arrives in the vicinity of comet 67 P/Churyumov- Gerasimenko and goes into orbit.
  • Rosetta observes the comet on its plunge toward the sun, deploying the lander
Rosetta

Credit: ESA Image

The Rosetta orbiter has eleven scientific instruments:

  • ALICE Ultraviolet Imaging Spectrometer
  • CONSERT Comet Nucleus Sounding
  • COSIMA Cometary Secondary Ion Mass Analyser
  • GIADA Grain Impact Analyser and Dust Accumulator
  • MIDAS Micro-Imaging Analysis System
  • MIRO Microwave Instrument for the Rosetta Orbiter
  • OSIRIS Rosetta Orbiter Imaging System
  • ROSINA Rosetta Orbiter Spectrometer for Ion and Neutral Analysis
  • RPC Rosetta Plasma Consortium
  • RSI Radio Science Investigation
  • VIRTIS Visible and Infrared Mapping Spectrometer
The Rosetta lander has nine scientific instruments:

  • APXS Alpha Proton X-ray Spectrometer
  • ÇIVA / ROLIS Rosetta Lander Imaging System
  • CONSERT Comet Nucleus Sounding
  • COSAC Cometary Sampling and Composition experiment
  • MODULUS PTOLEMY Evolved Gas Analyser
  • MUPUS Multi-Purpose Sensor for Surface and Subsurface Science
  • ROMAP RoLand Magnetometer and Plasma Monitor
  • SD2 Sample and Distribution Device
  • SESAME Surface Electrical and Acoustic Monitoring Experiment, Dust Impact Monitor
Lander

Credit: ESA Image

Posted in Asteroids, Comets, European Space Agency, Robotic Exploration, Space | Tagged: , , , , | 1 Comment »

LCROSS – IMPACT Imaged by Diviner on LRO

Posted by drdave on October 9, 2009

From the UCLA Diviner LRO blog:

The LRO Diviner instrument obtained infrared observations of the LCROSS impact this morning. LRO flew by the LCROSS Centaur impact site 90 seconds after impact at a distance of ~80 km. Diviner was commanded to observe the impact site on eight successive orbits, and obtained a series of thermal maps before and after the impact at approximately two hour intervals at an angle of approximately 48 degrees off nadir. In this viewing geometry, the spatial footprint of each Diviner detector was roughly 300 by 700 meters.

Diviner Impact Images of LCROSS

Credit: NASA / GSFC / UCLA

From the Planetary Society Blog:

preliminary, uncalibrated Diviner thermal maps of the impact site acquired two hours before the impact, and 90 seconds after the impact. The thermal signature of the impact was clearly detected in all four Diviner thermal mapping channels.

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

LCROSS – Impact

Posted by drdave on October 9, 2009

Images and Events of the final hour of the LCROSS mission.

3:42 – I MB data rate has been confirmed

3:43 – First Image from LCROSS Shepherding Spacecraft

3:48 – All Payload Instruments are Operating Nominally

3:59 – 3500 MPH at 3400 Miles from the Moon

4:23 – Poll of All Systems Ready for Observing Impact

4:31 – Impact of Centaur Stage

4:35 Impact of LCROSS Shepherding Spacecraft

A possible impact image in the infrared can be seen at the forum at NasaSpaceFlight.com.

Centaur After Separation

Centaur after Separation #1 with Low Data Rate Transmission

Centaur after Separation

Centaur after Separation #2 with Low Data Rate Transmission

First Image of Moon

First Image of Moon after High Data Rate Enabled

Image 2

Lunar Image

10 Minutes
10 Minutes Before Impact
Aim Point

Aim Point at Cursor Arrow

4 Minutes Infrared

4 Minutes Infrared Image

1 Minute Flash Mode

1 Minute – Transition to Flash Mode

30 Seconds30 Seconds 30 Seconds Infrared30 Seconds Infrared
15 Seconds Infrared15 Seconds Infrared 10 Seconds10 Seconds – Small Crater Visible at Top
LOSLoss of Signal It will be several days before the data has been calibrated and results begin to be released.

Credit: Screen Shots of NASA TV Images

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

LCROSS – Brace for Impact

Posted by drdave on October 8, 2009

LCROSS Impact

Credit: NASA Image

Tomorrow morning at 4:31:20 PDT (Phoenix time), the Centaur upper stage of the LRO mission will impact Cabeus crater on the Moon. At 4:35:39 the LCROSS instrument package will impact the Moon, having recorded the Centaur impact with a variety of imaging and spectroscopic instruments.

What are we looking for? WATER. Worth its weight in gold.

A complete list of events leading up to impact can be found at the LCROSS Flight Director’s Blog. Key events:

  • 01:00 PDT: Final orbit determination delivery for Separation(completed)
  • 17:00 PDT: Slow rotation to Separation attitude starts
  • 18:50 PDT: Separation
  • 19:30 PDT: Braking Burn starts (LCROSS)
  • 03:00 PDT: Start of Impact onboard command sequence
  • 3:36 PDT: Payload powers on
  • 4:10 PDT: Total Luminescence Photometer (TLP) Instrument powers on
  • 4:30:20 PDT: Flash Mode begins
  • 4:31:20 PDT: Centaur Impact
  • 4:31:23 PDT: Curtain Mode begins
  • 4:34:23 PDT: Crater Mode begins
  • 4:35:39 PDT: Shepherding Spacecraft impact

The latest LCROSS news can be found here.

Watch the LCROSS impact live starting at 3:30 PDT on NASA TV.

You can follow the live blog at NasaSpaceFlight. Current comments on the last page listed in the upper left.

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

The Augustine Commission – Postmortem – SPI Symposium

Posted by drdave on October 6, 2009

The Space Policy Institute at George Washington University hosted a half day symposium “Assessing The Options Of The Augustine Commission For Human Spaceflight” on 28 September 2009, and has now released the Notes and presentations.

Some of the participants in the Symposium (and their presentations) were:

Dr. Scott Pace, Director of the Space Policy Institute, began the proceedings by outlining the nine goals set for in the 2004 Presidential directives to NASA. Some have been, or will be, achieved:

  • Complete the International Space Station
  • Safely fly the Space Shuttle until 2010
  • No later than 2008, begin a series of robotic missions to Moon

Some are in danger:

  • Develop supporting innovative technologies, knowledge, and infrastructures
  • Promote international and commercial participation in exploration

And some will not be met:

  • Develop and fly the Crew Exploration Vehicle no later 2014
  • Return to Moon with goal of 2015 and no later than 2020
  • Aggressive in-situ resource program and robust precursor program
  • Sustained human presence on Moon for national preeminence, scientific and
    economic purposes, leading to Mars and other places

Dr. Pace reviewed the steadily declining budget provided NASA over the past five years (see the Sally Ride Slides – especially this). These cuts total approximately $42 Billion through 2020 versus the original ESAS (Exploration Systems Architecture Study) program, which topped out at $10 Billion per year in 2016 and is now expected to be only $6.5 Billion.

A critical observation was that “Budget Proposals are Policy”. Irrespective of what is said and written about America’s space policy, the budget dictates what can and cannot be done.”

Finally, Pace asked “Are there economically useful activities in space that can sustain human communities in space? Citing examples in the chart below, he concluded that we just do not know if there is anything in the upper right hand box.

Chart 1

The first panel of speakers was led by Gen. Lester Lyles (ret), a member of the Augustine Committee. His comments (see the Notes), centered around the task of the Commission. The Commission was tasked with assessing the following:

  • Present human spaceflight program
  • Future of Space Shuttle and ISS
  • The necessity of heavy lift
  • Crew access to low earth orbit and alternatives
  • Strategies and alternatives beyond low earth orbit

Major themes to be kept in mind included: safety, reliability, innovation, affordability, and sustainability.

Finally, Lyles summed up the key findings of the Commission:

  • NASA needs the right mission with the right size
  • Without an adequate budget there is no way that NASA can take on the great things it is asked to and maintain a viable program for space exploration
  • International partnerships should be addressed in greater detail than they are currently – there is lots of opportunities for greater partnerships and activities
  • Shuttle program should be extended, whether it be for a few flights or longer, it makes sense to consider any way to minimize gap
  • “Great nations do great things” – human spaceflight is a task worthy of a great nation
  • Extending ISS a “no brainer”– bottom line is we are just now completing space station and the U.S. and its international partners have only just begun to utilize scientific capabilities – Could be extended to 2025
  • NASA needs heavy lift capability – Looked at Ares 1, Ares V, and Ares V Light, but did not recommend one or the other; rather it depends on your objectives in space
  • Committee views COTS program favorably; it should be continued – Strong potential for commercial space sector to service ISS
  • A non-mission specific, basic space technology program should be established to support exploration
  • There are human spaceflight pathways to Mars – Mars is the ultimate destination, but may not be the first
  • Committee laid out alternatives for Moon and Mars and defined risks as best as they could

Tom Young, former CEO of Martin-Marietta, spoke next. One of his major themes was that the current situation was being driven by budget, and that the decisions made today will influence the course of space exploration for the rest of the century. He hoped that following the great adventure of the twentieth century – landing on the Moon and returning – the twenty-first century would not be remembered for “we saved $3 Billion dollars”.

Quoting from the analysis by Dwayne Day at The Space Review:

Young also warned that in order for NASA to be a smart buyer and to ensure success, the agency needed in-house systems engineering talent. Echoing Scott Pace’s earlier comments, he said that during the 1990s the United States engaged in a number of “acquisition reforms,” including the Air Force’s reduction of oversight of contractor operation of launch vehicles like the Titan IV as well as some of the aspects of NASA’s “faster, better, cheaper” program. (Author’s note: Young was clear that he was not criticizing faster, better, cheaper in its entirety.) “We just fired all of the experienced people,” Young said, and adopted a policy that “government would sit in the back of the room” and let the contractors run the show. “That was a horrible mistake. The net result of that experiment was $11.2 billion in failures. We tried that experiment, it was a horrible failure.”

Young finished by echoing previous speakers that human space flight was a policy issue, not a budget issue. He would quote Lyles: “Great Nations do Great Things”.

Next up was Dr. Doug Stanley, who has worked at NASA and Orbital Sciences Corporation, and is currently from Georgia Tech. One of the items he discussed was the idea that the assumptions made by NASA have driven the designs. For example, if the Crew Exploration Vehicle (CEV) had not been required to go to the ISS, then the Moon mission would have been best accomplished with a dual launch of two identical rockets and an EOR-LOR strategy (Earth Orbit Rendezvous – Lunar Orbit Rendezvous). A single Shuttle Derived Launch Vehicle would be the most cost effective solution for the heavy lift requirements. But it would not be cost effective for ISS purposes.

On the other hand, if the focus had been solely on servicing the ISS, then commercial Evolved Expendable Launch Vehicles (EELV – Delta IV) would have been selected. It would have been cheaper and quicker to operational status than building a new rocket.

Instead, NASA had to satisfy both objectives. And therefore, chose to develop two new rockets (new engines, new tanks, new solid rocket motors). This was the riskiest and most expensive course.

Young concludes with two sets of recommendations:

White House should immediately decide on:

  • ISS extension through 2020
  • Shuttle extension into 2011 and/or beyond 2011
  • Beyond-LEO human mission destination(s) and time-frame
  • Out-year available budget
  • General policy towards commercial and international ISS crew transport

NASA should be allowed to then define design reference mission(s) and requirements and perform ESAS-like architecture study to:

  • Perform apples-to-apples cost/safety/risk comparison of Augustine-defined options and selected other combinations of options
  • Re-visit EELV/SDV trades – including side-mount
  • Perform detailed definition and economic analysis of propellant depots
  • Determine true cost/risk of “commercial” crew transport
  • Examine workforce impacts of options
  • Define more detailed budgets to support 2011 budget cycle

[Ed: One has to look back at Young's comment above about NASA thinking that a SDLV "...would not be cost effective for ISS purposes" and wonder why they did not realize that the SDLV would only need to be used for a year or so until EELV could come on line for ISS and other LEO missions. The implication is that EELV would have been cheaper than Ares I, and SDLV would have been cheaper than Ares V.]

The second panel discussion, on science and international relations, was begun by Paul Spudis from the Lunar and Planetary Institute.

Dr. Spudis fundamentally disagrees with the “Four Canons” of the Space Program, enshrined in the Summary Report of the Augustine Commission:

  • Mars is the ultimate destination
  • Heavy-lift is a requirement
  • It is necessary to get the public excited
  • There is no problem at NASA that money cannot fix

He contrasts the Current Template with the Desired Template:

Current Template:

  • Custom-built, self-contained, mission specific spacecraft
  • Launch on expendable vehicles
  • Operate for set lifetime
  • Abandon after use
  • Repeat

Desired Template:

  • Incremental, extensible building blocks
  • Extract material and energy resources of space to use in space
  • Launch only what cannot be fabricated or built in space
  • Build and operate flexible, modular, extensible in-space systems
  • Maintain, expand and use indefinitely

Obviously, Dr. Spudis takes the Long View: “My objective is to move humanity into outer space. How do you do that? By living off the land.” He wants to find opportunities in the upper right corner of Pace’s matrix.

Next up was Tom Jones, with the Association of Space Explorers and a former astronaut. His comments are summed up nicely in the abstract to the paper he presented:

By conducting a series of piloted Near-Earth Object (NEO) missions beginning about 2020, the U.S. will reinforce the scientific, economic, programmatic, operations, planetary defense, and public outreach elements of its human exploration program. Astronauts exploring a NEO would provide synergistic scientific return from a new “planetary” surface, substantially different in origin, age, and composition from those of the Moon or Mars. Explorers would assay NEO resources vital to future U.S. economic activity in space, and demonstrate extraction and utilization techniques for water, volatiles, and valuable metals. Piloted missions will also provide structural and civil engineering data needed for future deflection of hazardous NEOs. Impact prevention is a common sense, “know your enemy” mission for human explorers; the public will support space-based efforts to better understand and prevent a damaging NEO collision with Earth. Astronaut expeditions to NEOs offer dramatic, high-profile opportunities to engage the public in ground-breaking exploration more than a million miles from Earth. Finally, in the event U.S. plans for a lunar return are delayed, NEOs offer a challenging suite of alternative destinations. Easier to reach than the Moon’s surface, NEOs will nevertheless broaden U.S. space capabilities, demonstrate a firm commitment to ambitious human space activities, and increase momentum toward the eventual exploration of Mars.

Dr. John Logsdon lead of his comments on the International Space Station and International cooperation by quoting Secretary of State Hillary Clinton, 16 July 2009:

“Our approach to foreign policy must reflect the world as it is, not as it used to be. It does not make sense to adapt a 19th-century concert of powers or a 20th-century balance-of-power strategy. We cannot go back to Cold War containment or to unilateralism. . . . We will lead by inducing greater cooperation among a greater number of actors and reducing competition, tilting the balance away from a multi-polar world and toward a multi-partner world.”

Dr. Logsdon advocated including India and China in multi-lateralization of space. The question in his mind was whether there would be Presidential leadership.

For the international perspective, Dr. Alain Dupas, Director of Strategic Studies at the Paris-based College de Polytechnique, presented his views on the Augustine Committee’s recent report. Europe, he said, has been under the impression that the United States had made a firm decision regarding it’s exploration program. Now, there are serious concerns about America changing its mind. Fortunately, he noted, the ISS would be supported at least through 2020. This bodes well for the discussions about the Global Exploration Strategy. Dupais noted that the Flexible Path option offered “interesting opportunities for Europe”.

Mr. Brett Alexander, from the Commercial Spaceflight Federation, led the third panel of the morning on security and commerce. One of the main points he made was that the Augustine Commission had fallen into a false dichotomy: having to choose between Ares I and commercial EELV access to space. The real issue is choosing Ares I or the International Space Station. NASA does not have the budget for both.

Finally, with regard to safety, Alexander noted that Astronauts will not fly on unproven commercial vehicles, and notes ironically that:

  • The Atlas V has a long and proven track record, and the team that puts it together and launches has a demonstrated track that goes beyond the vehicle itself.
  • Falcon 9 and Taurus II will have conducted multiple cargo flights to ISS under COTS prior to being permitted to ferry human crew to LEO
  • Contrast this with the fact that Ares 1X/1 will have completed only two test flights prior to being permitted to carry crew to LEO

Eric Sterner spoke next. He is a former Republican House Armed Services Committee staffer and currently a fellow at the Marshall Institute. He made several points concerning international cooperation as a policy decision. First, that “International cooperation is useful but policy makers should be aware international partnerships have risks. You inherit or import into your program all their bureaucracy, all the budget woes. ISS proves you can do it, but it took us 25 years.” And second, considering China. “How would the U.S. deal with human rights issues if China were a partner in space exploration? It matters what values you take into space. How do you deal with proliferation issues? The Clinton administration threatened to cut off space-related payments to the Russia for its proliferation behavior with Iran”.

Next to last was Robert Read from the Office of the Undersecretary of Defense. His remarks addressed the implications of NASA and space exploration for the Solid Rocket Motor industry. Historically, the Department of Defense (DoD) has relied on solid rocket motors for land base Minuteman III ICBM and sea launched Trident II D-5, as well as many other weapon systems. He notes that DoD is concerned that shutting down the Shuttle and SDLV programs will so shrink the market that the program might collapse. He points out that:

  • One Shuttle stack is equivalent to 10 Trident II D-5 and 17 Minuteman III missiles in terms of solid propellant weight
  • The DoD is concerned over the potential loss of SRM suppliers once the Shuttle is retired
  • The DoD will be studying the issue further, given the national security implications of further decline of the SRM industrial base.

From The Space Review article, Read’s comments concerning how delicate the industry is at the moment:

He recounted how a few years ago a small company was going to move its operations from Texas overseas. The company’s motivation was that 95% of its business was commercial and the government accounted for only 5% of its business. But moving its manufacturing overseas would have required the government to recertify all of the company’s components, at a cost of hundreds of millions of dollars to the DoD, and ultimately the American taxpayers.

Finally, John Karas of Lockheed Martin addressed the workforce issues. A major concern is the loss of talent. 35% of the workforce is eligible for retirement right now. Industry needs to see NASA with a realistic goal and adequate funding in order to attract new, young talent to learn from the old guard before they retire. America’s heavy lift capability is unmatched elsewhere, and will remain so. But it can, and is currently, slipping away with the confusion and disarray of the space policy and budget problems.

So what do we garner from this long discussion? The debate is a tug of war in many dimensions: practical, political, monetary and technical.

I would like commercial crew launch to Low Earth Orbit and the ISS, a single Shuttle Derived Heavy lift vehicle and propellant depots. But that’s just my opinion.

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