The first libration-point satellite - Mission overview and flight history
Abstract
On August 12, 1978, a scientific spacecraft called International Sun-Earth Explorer-3 (ISEE-3) was launched towards the interior sun-earth libration point, L1. The spacecraft was placed into a 'halo orbit' around the L1 point on November 20, 1978, thus becoming the first libration-point satellite. During its 100-day transfer trajectory, ISEE-3 lingered in a region where the gravitational effects of the sun and the earth are comparable, leading to some interesting tradeoffs concerning the maneuver strategy for halo-orbit insertion. Following orbit insertion, stationkeeping maneuvers were required to maintain the delicate equilibrium in the halo orbit. Details are presented for all of the velocity change maneuvers that were executed prior to the completion of the first halo orbit on May 14, 1979. Orbit selection, trajectory design, and the scientific objectives of the ISEE-3 mission are also discussed.
- Publication:
-
American Institute of Aeronautics and Astronautics Conference
- Pub Date:
- June 1979
- Bibcode:
- 1979aiaa.confU....F
- Keywords:
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- Explorer 3 Satellite;
- Gravitational Effects;
- Libration;
- Spacecraft Trajectories;
- Trajectory Analysis;
- Transfer Orbits;
- Design Analysis;
- Halo Orbit Space Station;
- Interplanetary Trajectories;
- Orbit Calculation;
- Orbital Mechanics;
- Space Missions;
- Spacecraft Maneuvers;
- Stationkeeping;
- Astrodynamics