Print Email Facebook Twitter A semi-analytical method for computing third-body effects on earth's and lunar satellite orbits Title A semi-analytical method for computing third-body effects on earth's and lunar satellite orbits Author van de Graaff, R.C. Faculty Aerospace Engineering Date 1977 To reference this document use: http://resolver.tudelft.nl/uuid:2abab3c5-25d7-4190-918a-6af9b42fcf80 Publisher Delft University of Technology Source Delft University of Technology, Department of Aerospace Engineering, Report LR-231 Part of collection Institutional Repository Document type report Rights (c) 1977 Delft University of Technology Files PDF LR-231.pdf 1.2 MB Close viewer /islandora/object/uuid:2abab3c5-25d7-4190-918a-6af9b42fcf80/datastream/OBJ/view