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Before the end of the NASA TV broadcast, they gave a tentative lift-off time of 9:45 AM Eastern. That would be 8:45 AM Central.
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Hanlon's Razor - "Never attribute to malice that which can be adequately explained by stupidity." Asimov's addition - "Or ignorance." "On two occasions, I have been asked [by members of Parliament], 'Pray, Mr. Babbage, if you put into the machine wrong figures, will the right answers come out?' I am not able to rightly apprehend the kind of confusion of ideas that could provoke such a question." -- Charles Babbage |
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Thank you!
So it will be at 8:45 tomorrow? Or was it supposed to be 8:45 today. If the later is true, at what time then would it be launched tomorrow, if anyone knows.
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May the schwartz be with you! |
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I heard on the radio coming to work this morning -- they were having problems with some fuel sensors. The first thing I thought of: is it the sensor itself, or my telemetry circuit gone bad.
So far, no word from LockMart, so I suppose our equipment is working OK, and it really is the actual sensor(s). I hope they figure it out. When does the overall 2005 Mars "window" close? Sometime in September?
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From NASA HQ:
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Does the MRO need to be in an equitorial parking orbit before the Trans Martian Injection burn? If so, does it get to a zero inclination orbit as part of the orbital insertion?
I can't seem to visualize an Earth-Mars transfer with the high Earth orbital inclination associated with launching from KSC. The only thing I can think of is the first Centaur burn is done over the equator and equitorializes the parking orbit. |
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MRO launch coverage from NASA TV has started. The NASA and Lockheed polls for the 4 minute hold are both GO. Count is restarting.
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In the progress of this discussion I shall endeavor to give a satisfactory answer to all the objections which shall have made their appearance, that may seem to have any claim to your attention. Alexander Hamilton, Federalist No. 1 |
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So far, so good - Atlas has seperated and Centaur is burning. Payload seperation next up.
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In the progress of this discussion I shall endeavor to give a satisfactory answer to all the objections which shall have made their appearance, that may seem to have any claim to your attention. Alexander Hamilton, Federalist No. 1 |
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From Spaceflight Now
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Cool.
By the way CRRES was truly a joint mission. Our contract was with NASA to build the spacecraft, but the AF provided much of the funding and the AF payloads. NASA provided the launch vehicle and the NASA payloads. Mission operations were from an AF facility. |
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Mars Reconnaissance Orbiter Mission Status August 18
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Calibration Image of Earth by (MRO) Mars Color Imager
(I wonder why it's on a JPL MER page.) ![]() It ain't much to look at. Quote:
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Found on the web.
http://www.planet4589.org/ The latest (issue no. 552) contains this excellent info on MRO NASA's latest Mars mission was launched on Aug 12. MRO is twice the mass of other recent Mars missions, 2180 kg at launch - back to the scale of the ambitious but unsuccessful Mars Observer whose failure helped triggered creation of the `faster, better, cheaper' missions of the 1990s. The big spacecraft carries a big camera, the 0.5 meter aperture HiRISE telescope, which will return high resolution images of the surface, and a big 3-meter communications dish to allow a high data rate for sending the pictures back. MRO has 1196 kg of hydrazine propellant, with six 170-Newton MR-107E Aerojet thrusters and six smaller 22-Newton MR-160E thrusters. The mutiple engines provide propulsion for course correction and Mars orbit insertion. MRO will reach Mars in March 2006. The NASA Mars Program --------------------- Spacecraft Launch Mass NASA Program Mariner 3 1964 Nov 5 261 kg Mariner flyby (failed) Mariner 4 1964 Nov 28 261 kg Mariner flyby Mariner 6 1969 Feb 25 385 kg Mariner flyby Mariner 7 1969 Mar 27 383 kg Mariner flyby Mariner 8 1971 May 9 1031 kg Mariner orbiter (failed) Mariner 9 1971 May 30 1031 kg Mariner orbiter Viking 1 1975 Aug 20 3534 kg Viking orbiter/lander Viking 2 1975 Sep 9 3526 kg Viking orbiter/lander Mars Observer 1992 Sep 25 2565 kg Planetary Observer, failed Mars Global Surveyor 1996 Nov 7 1062 kg Mars Surveyor Program Mars Pathfinder 1996 Dec 4 880 kg Discovery Program Mars Climate Orbiter 1998 Dec 11 629 kg Mars Surveyor Program, failed Mars Polar Lander 1999 Jan 3 615 kg Mars Surveyor Program, failed 2001 Mars Odyssey 2001 Apr 7 730 kg Mars Surveyor Program Mars Exploration Rover A 2003 Jun 10 1062 kg Mars Program Mars Exploration Rover B 2003 Jul 8 1062 kg Mars Program Mars Reconnaissance Orbiter 2005 Aug 12 2180 kg Mars Program Launch of MRO was with a Lockheed Martin Atlas V, model 401, serial AV-007. The Atlas CCB stage fired for 4 minutes, followed by the first Centaur stage burn, putting MRO in a 148 x 185 km x 28.5 deg Earth parking orbit 14 min after launch. Centaur fired again at 1132 UTC to reach escape velocity, and separated from MRO at 1141 UTC, with both vehicles on hyperbolic Earth departure orbit with around 205 km perigee and 40.7 deg inclination. MRO passed lunar orbit on Aug 13 and is now in a 1.013 x 1.680 AU x 3.1 (ecliptic) deg heliocentric transfer orbit to Mars. The Centaur is lagging slightly behind in a 1.013 x 1.659 AU orbit, targeted to miss Mars. |
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The Nuts and Bolts
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Everything I need to know I learned through Googling. |