scholarly journals Minimum-Fuel Low-Earth-Orbit Aeroglide and Aerothrust Aeroassisted Orbital Transfer Subject to Heating Constraints

2018 ◽  
Vol 55 (3) ◽  
pp. 723-748 ◽  
Author(s):  
Reagan Fuhr ◽  
Anil V. Rao
Keyword(s):  
Low Earth Orbit ◽  
Earth Orbit ◽  
Orbital Transfer ◽  
Aeroassisted Orbital Transfer

Orbital transfer vehicle (OTV) system sizing study for manned GEO satellite servicing

2016 ◽  
Vol 120 (1226) ◽  
pp. 573-599 ◽  
Author(s):  
B. Chudoba ◽  
G. Coleman ◽  
L. Gonzalez ◽  
E. Haney ◽  
A. Oza ◽  
...  
Keyword(s):  
Low Earth Orbit ◽  
Geostationary Orbit ◽  
Earth Orbit ◽  
Orbital Transfer ◽  
Geo Satellite ◽  
Satellite Servicing ◽  
Geo Satellites ◽  
Kennedy Space ◽  
Cost Factors ◽  
Concept Of Operations

ABSTRACTIn an effort to quantify the feasibility of candidate space architectures for astronauts servicing Geosynchronous Earth Orbit (GEO) satellites, a conceptual assessment of architecture-concept and operations-technology combinations has been performed. The focus has been the development of a system with the capability to transfer payload to and from geostationary orbit. Two primary concepts of operations have been selected: (a) Direct insertion/re-entry (Concept of Operations 1 – CONOP 1); (b) Launch to low-earth orbit at Kennedy Space Center inclination angle with an orbital transfer to/from geostationary orbit (Concept of Operations 2 – CONOP 2). The study concludes that a capsule and de-orbit propulsion module system sized for the geostationary satellite servicing mission is feasible for a direct insertion/re-entry concept of operation CONOP 1. Vehicles sized for CONOP 2 show overall total mass savings when utilising the aero-assisted orbital transfer vehicle de-orbit propulsion module options compared to the pure propulsive baseline cases. Overall, the consideration of technical, operational and cost factors determine if either the aero-assisted orbital transfer vehicle concepts or the re-usable/expendable ascent/de-orbit propulsion modules is the preferred option.

Robust orbital transfer for low earth orbit spacecraft with small-thrust

2010 ◽  
Vol 347 (10) ◽  
pp. 1863-1887 ◽  
Author(s):  
Xuebo Yang ◽  
Huijun Gao ◽  
Peng Shi
Keyword(s):  
Low Earth Orbit ◽  
Earth Orbit ◽  
Orbital Transfer

A three-dimensional wake model for low earth orbit

1983 ◽  
Author(s):  
I. KATZ ◽  
D. COOKE ◽  
D. PARKS ◽  
M. MANDELL ◽  
A. RUBIN
Keyword(s):  
Three Dimensional ◽  
Low Earth Orbit ◽  
Earth Orbit ◽  
Wake Model
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