When LADEE launched on September 6, it launched into Earth orbit. Today, it is finally on a path that will take it to its October 6 lunar orbit insertion. A direct-to-the-Moon trajectory would have been faster, but it would have required much more fuel and a larger launch vehicle.
I've been wondering about the status of LADEE and Lunar Reconnaissance Orbiter -- two missions not managed by JPL or APL -- in the face of the shutdown. I have finally been pointed to a great source of information on LADEE's status, thanks to a comment left on my blog entry by Mike Loucks yesterday: "LADEE is being operated by essential personnel at NASA/Ames. TCM-1 was executed Tuesday afternoon as planned, as will be the Lunar Orbit Insertion Burns that start on Sunday." In a series of posts on their blog "The Astrogator's Guild," spacecraft navigators Mike Loucks and John Carrico, Jr. have been explaining LADEE's circuitous path to the Moon.
First, a quick reminder on some basic orbital mechanics. With a spacecraft in an elliptical orbit, it is sometimes very far from the planet and sometimes very close to it. The far point is the orbital apoapsis, and the close point is the periapsis. When a spacecraft is orbiting Earth, these points are usually referred to as apogee and perigee. Another thing about elliptical orbits: spacecraft are moving much faster when they are near periapsis than when near apoapsis. So a spacecraft on an elliptical orbit spends much more of its time far away from the planet, near apoapsis, than it spends close to the planet, near periapsis.
Here is what LADEE's initial orbit looked like on the morning of September 11, 2013. The green path had already been traveled by the spacecraft (green circle); it had passed through apoapsis and was returning toward Earth. The dotted lines show the spacecraft's future path.
Mike Loucks and John Carrico
LADEE's orbit on September 11, 2013
As explained further on their blog, LADEE performed two Perigee Maneuvers on September 13 and 21, firing its main engine to increase its speed as it passed through perigee. This has the effect of raising the height of the orbit's apogee. The second Perigee Maneuver gave LADEE the orbital height needed to reach the Moon, but the Moon wasn't there at the time that it arrived at its next apogee. LADEE returned on a last Earthward loop, reaching its final perigee yesterday at 11:00 UTC. It is now on the way to the Moon, which will be at the right spot in its orbit this time for LADEE to rendezvous with it.
LOI-1 is designed to place the spacecraft into a 24 hr orbit, with a periselene altitude of 750 590 km. After 3 revolutions in this orbit, 3rd-body Earth gravitational perturbations will have lowered periselene to an altitude of 250 km (by design). At this point, LOI-2 will be performed on 9 Oct 2013 10:37 UTC ( to place LADEE into a 4 hr orbit (also with a 250 km periselene altitude). LADEE will spend 3 days in this orbit until LOI-3 (12 Oct 2013 10:37 UTC), which circularizes the orbit at 250 km. LADEE will spend 30 days in this “commissioning orbit”, and will also perform tests using the laser communications experiment (LLCD). The timing and magnitudes of the maneuvers leading to the commissioning orbit are given below.
AM1 11 Sep 2013 23:00:00.000 9.34 m/sec
PM1 13 Sep 2013 16:36:08.000 16.96 m/sec
PM2 21 Sep 2013 11:53:19.000 17.492 m/sec
TCM1 01 Oct 2013 22:00:00.000 0.9 m/sec [now completed]
LOI1 06 Oct 2013 10:57:00.210 329.86 m/sec
LAM1 07 Oct 2013 22:51:32.205 0 m/sec (error corrections for LOI-1)
LOI2 09 Oct 2013 10:37:55.651 295.99 m/sec
LOI3 12 Oct 2013 10:37:34.993 238.56 m/sec
LADEE's orbit on September 28, 2013
Go LADEE! And I hope that by the time you reach the Moon, this stupid shutdown will be over and scientists employed at NASA centers can get on with the science!!