Document information
- University
- Politecnico di Milano
- Degree programme
- Aerospace Engineering
- Subject
- Introduzione all'analisi di Missioni Spaziali
- Classification
- Exercises · Complete set
- Original format
- Text
- Searchable text
← Back
ExercisesComplete set
Complete exercise of the course
Study material for Introduzione all'analisi di Missioni Spaziali, shared by the Studwiz community and reviewed by moderators.
Introduzione all'analisi di Missioni SpazialiComplete set
Document information
What's included in this study material
Study material for Introduzione all'analisi di Missioni Spaziali, shared by the Studwiz community and reviewed by moderators.
Import quality: text was extracted directly from the original document.
Extracted content from the document
Representative passages recognised in different parts of the material. The full extracted text remains available to search, while this compact preview makes the page easier to read.
Page 1
Introduzione all’analisi di missioni spazialiesercizi Esercitazione 1 3 µ = 398.600,433Km 52 Rt= 6378km ° ORBITAGEOSTAZIONARIA: T= 24h (ORBITACIRCOLAREEQUATORIALE) ° 2'KEPLERO: T= 2T a> a= , TZU= 42' 241KM = P= t ⊥ 4ITL . h= t- rt = 35 ' 861KM E= 1 ✓2- 1 { 2 t v = zur 1 - 1 = M = 3,07knls E= - vu t za t za RT 0 tcos) = Rt )= arccos Rt = 81,3t t Rt= 6378 km ° Zp= 300 km za = 2000 km tp= 6678 km ta= 8378Km e a= tat tp = 7528km 2 . E = ta- tp = 0,1129 l'atto . p= a11- EZ)= 7432 km . T= 2T 23= 6500,35 ^ . vp= ~ 11te )= 8,13knls va= 1 11- e)= 6,52knls p p 2= 10 " 000 KM E = 0, 1129 . p= a11- CZ)= 9872, 5 km . rp = P = 8871 km tra= P = 11.129KM 1te 1- e . T= 2A 23= 99525 → . vp= 1 (1te )= 7,07 1 knls va= 1 (1- e)= 5,637knls p p 1-p= 6678Km a= 20.000km tp= p 1 te . ( pp= aii.e) e = µ. rp = o.gg, p= a.11- CZ) a ° p= a(1- CZ)= 11 ' 126,2km - . -
Preview
First page of the document.