Artist's interpretation of the GRAIL tandem spacecraft above the lunar surface.
|Operator||NASA / JPL|
|COSPAR ID||2011-046 (A, B)|
|SATCAT no.||37801, 37802|
|Mission duration||1 year, 3 months, 7 days, 9 hours|
|Manufacturer||Massachusetts Institute of Technology, LMSS|
|Launch mass||307 kg (677 lb)|
|Dry mass||132.6 kg (292 lb)|
|Power||(Solar array / Li-ion battery)|
|Start of mission|
|Launch date||September 10, 2011, 13:08:52.775UTC|
|Rocket||Delta II 7920H-10 D-356|
|Launch site||Cape Canaveral SLC-17B|
|Entered service||December 31, 2011 (Ebb)|
January 1, 2012 (Flow)
|Semi-major axis||1,788.0 kilometres (1,111.0 mi)|
|Periselene altitude||25 kilometres (16 mi)|
|Aposelene altitude||86 kilometres (53 mi)|
|Impact date||GRAIL A: December 17, 2012, 22:28:51 UTC|
|Impact date||GRAIL B: December 17, 2012, 22:29:21 UTC|
The Gravity Recovery and Interior Laboratory (GRAIL) was an American lunar science mission in NASA's Discovery Program which used high-quality gravitational field mapping of the Moon to determine its interior structure. The two small spacecraft GRAIL A (Ebb) and GRAIL B (Flow) were launched on 10 September 2011 aboard a single launch vehicle: the most-powerful configuration of a Delta II, the 7920H-10. GRAIL A separated from the rocket about nine minutes after launch, GRAIL B followed about eight minutes later. They arrived at their orbits around the Moon 25 hours apart. The first probe entered orbit on 31 December 2011 and the second followed on 1 January 2012. The two spacecraft impacted the Lunar surface on December 17, 2012.
Maria Zuber of the Massachusetts Institute of Technology is GRAIL's principal investigator. NASA's Jet Propulsion Laboratory manages the project. As of August 5, 2011[update], the program had cost US$496 million. Upon launch the spacecraft were named GRAIL A and GRAIL B and a contest was opened to school children to select names. Nearly 900 classrooms from 45 states, Puerto Rico and the District of Columbia, participated in the contest. The winning names, Ebb and Flow, were suggested by 4th grade students at Emily Dickinson Elementary School in Bozeman, Montana.
Each spacecraft transmitted and received telemetry from the other spacecraft and Earth-based facilities. By measuring the change in distance between the two spacecraft, the gravity field and geological structure of the Moon was obtained. The two spacecraft were able to detect very small changes in the distance between one another. Changes in distance as small as one micrometre were detectable and measurable. The gravitational field of the Moon was mapped in unprecedented detail.
- Map the structure of the lunar crust and lithosphere
- Understand the asymmetric thermal evolution of the Moon
- Determine the subsurface structure of impact basins and the origin of lunar mascons
- Ascertain the temporal evolution of crustal brecciation and magmatism
- Constrain the deep interior structure of the Moon
- Place limits on the size of the Moon's inner core
The data collection phase of the mission lasted from 7 Mar 2012 to 29 May 2012, for a total of 88 days. A second phase, at a lower altitude, of data collection began 31 Aug 2012, and was followed by 12 months of data analysis. On 5 Dec 2012 NASA released a gravity map of the Moon made from GRAIL data. The knowledge acquired will aid understanding of the evolutionary history of the terrestrial planets and computations of lunar orbits.
- Ka band Lunar Gravity Ranging System (LGRS), derived from the Gravity Recovery and Climate Experiment instrument. 90% of the GRACE software was reused for GRAIL.
- Radio science beacon (RSB)
- Moon Knowledge Acquired by Middle school students (MoonKAM). Each MoonKAM system (one per spacecraft) consists of a digital video controller and four camera heads. Click here  for a MoonKAM photo from lunar orbit.
Thrusters aboard each spacecraft were capable of producing 22 newtons (4.9 lbf). Each spacecraft was fueled with 103.5 kilograms (228 lb) of hydrazine to be used by the thrusters and main engine to enable the spacecraft to enter lunar orbit and transition to the science phase of its mission. The propulsion subsystem consisted of a main fuel tank and a Re-repressurization system which were activated shortly after lunar orbit insertion.
|Attempt||Planned||Result||Turnaround||Reason||Decision point||Weather go (%)||Notes|
|1||8 Sep 2011, 8:37:06 am||scrubbed||—||high level winds||8 Sep 2011, 8:30 am||40%||A weather balloon was released minutes before the decision point to take the latest readings of upper level winds and Air Force weather reconnaissance aircraft were aloft beginning at 7 am.|
|2||8 Sep 2011, 9:16:12 am||scrubbed||0 days, 0 hours, 39 minutes||high level winds||8 Sep 2011, 9:07 am||40% ||Range was reconfigured for omni antennae instead of tracked ones to support 99 degree azimuth.|
|3||9 Sep 2011, 8:33:25 am||abandoned||0 days, 23 hours, 17 minutes||rocket propulsion||40%||An issue with the rocket's propulsion system was detected while the Delta 2 rocket was drained of fuel.|
|4||10 Sep 2011, 8:29:45 am||scrubbed||0 days, 23 hours, 56 minutes||high level winds||10 Sep 2011, 8:21 am||60%|
|5||10 Sep 2011, 9:08:52 am||Success||0 days, 0 hours, 39 minutes|
GRAIL awaits launch at Cape Canaveral Air Force Station.
Unlike the Apollo program missions, which took three days to reach the Moon, GRAIL made use of a three- to four-month low-energy trans-lunar cruise well outside the Moon's orbit and passing near the Sun-Earth Lagrange point L1 before looping back to rendezvous with the Moon. This extended and circuitous trajectory enabled the mission to reduce fuel requirements, protect instruments and reduce the velocity of the two spacecraft at lunar arrival to help achieve the extremely low 50 km (31 mi) orbits with separation between the spacecraft (arriving 25 hours apart) of 175 to 225 km (109 to 140 mi). The very tight tolerances in the flight plan left little room for error correction leading to a launch window lasting one second and providing only two launch opportunities per day.
The primary science phase of GRAIL lasted for 88 days, from 7 Mar 2012 to 29 May 2012. It was followed by a second science phase starting on 8 Aug.
The orbital insertion dates were December 31, 2011(for GRAIL-A) and January 1, 2012 (for GRAIL-B).
The spacecraft were operated over the 88-day acquisition phase, divided into three 27.3 day long nadir-pointed mapping cycles. Twice each day there was an 8-hour pass in view of the Deep Space Network for transmission of science and "E/PO MoonKam" data.
Final experiment and mission end
At the end of the science phase and a mission extension, the spacecrafts were powered down and decommissioned over a five-day period. The spacecraft impacted the lunar surface on December 17, 2012. Both spacecraft impacted an unnamed lunar mountain between Philolaus and Mouchez at . Ebb, the lead spacecraft in formation, impacted first. Flow impacted moments later. Each spacecraft was traveling at 3,760 miles per hour (1.68 km/s). A final experiment was conducted during the final days of the mission. Main engines aboard the spacecraft were fired, depleting remaining fuel. Data from that effort will be used by mission planners to validate fuel consumption computer models to improve predictions of fuel needs for future missions. NASA has announced that the crash site will be named after GRAIL collaborator and first American woman in space, Sally Ride.
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- GRAIL: Mission NASA
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