{
  "annotation_id": "53870990-b0b5-4eb2-b1c2-23e15cb41a08",
  "date_created": "2026-03-02T18:01:04.393000Z",
  "date_modified": "2026-03-02T18:01:04.393000Z",
  "file_hash": "34e247752f29a312c6f136c97298a7cdd300fc64850f441a3f459cbb9bf37d5e",
  "private": false,
  "record": {
    "abstract": "Placing satellites in geostationary obital (GEO) is propellant exigeant. It\nrequires large propellant consumption that will take a large part of the total\nmass. Hence the interest is reduce the mass of propellant loaded both in the\nrocket and the satellite. Both for improving selection of transfer orbits and\npropellant.\n  In this paper we give a reiew of analysis of launching of satellite to GEO\nusing multistage transfer orbit in order to reduce the mass of propellant.\nMaking this analysis complete, the effect of the general relativity regarding\nelliptical transfer orbit and its potensial utilization will be briefly\nreviewed.",
    "arxiv_id": "physics/0511114",
    "authors": [
      "S. Ng"
    ],
    "categories": [
      "physics.space-ph"
    ],
    "title": "Analyze of multistage transfer orbit to reach the GEO orbit in a   rotational symmetric gravitational field",
    "url": "https://arxiv.org/abs/physics/0511114"
  },
  "schema_id": "dorsal/arxiv",
  "source": {
    "execution_id": "7aba1326-8061-4f54-afba-5d5ad3b7bac2",
    "id": "arXiv Dataset IDs",
    "type": "Model",
    "variant": "snapshot-2026-03-01",
    "version": "0.1.0"
  },
  "user_id": 1000002
}