9 research outputs found
Active space debris removal by a hybrid propulsion module
During the last 40 years, the mass of the artificial objects in orbit increased quite steadily at the rate of about 145 metric tons annually, leading to a total tally of approximately 7000 metric tons. Now, most of the cross-sectional area and mass (97% in LEO) is concentrated in about 4600 intact objects, i.e. abandoned spacecraft and rocket bodies, plus a further 1000 operational spacecraft. Simulations and parametric analyses have shown that the most efficient and effective way to prevent the outbreak of a long-term exponential growth of the catalogued debris population would be to remove enough cross-sectional area and mass from densely populated orbits. In practice, according to the most recent NASA results, the active yearly removal of approximately 0.1% of the abandoned intact objects would be sufficient to stabilize the catalogued debris in low Earth orbit, together with the worldwide adoption of mitigation measures. The candidate targets for removal would have typical masses between 500 and 1000 kg, in the case of spacecraft, and of more than 1000 kg, in the case of rocket upper stages. Current data suggest that optimal active debris removal missions should be carried out in a few critical altitude-inclination bands. This paper deals with the feasibility study of a mission in which the debris is removed by using a hybrid propulsion module as propulsion unit. Specifically, the engine is transferred from a servicing platform to the debris target by a robotic arm so to perform a controlled disposal. Hybrid rocket technology for de-orbiting applications is considered a valuable option due to high specific impulse, intrinsic safety, thrust throttle ability, low environmental impact and reduced operating costs. Typically, in hybrid rockets a gaseous or liquid oxidizer is injected into the combustion chamber along the axial direction to burn a solid fuel. However, the use of tangential injection on a solid grain Pancake Geometry allows for more compact design of the propulsion unit. Only explorative tests were performed in the past on this rocket configuration, which appears to be suitable as de-orbiting system of new satellites as well as for direct application on large debris in the framework of a mission for debris removal. The paper describes some critical aspects of the mission with particular concern to the target selection, the hybrid propulsion module, the operations as well as the systems needed to rendezvous and dock with the target, and the disposal strateg
System Analysis of Space Missions [ΠΠ»Π΅ΠΊΡΡΠΎΠ½Π½ΡΠΉ ΡΠ΅ΡΡΡΡ] : electronic lecture notes
ΠΡΠΏΠΎΠ»ΡΠ·ΡΠ΅ΠΌΡΠ΅ ΠΏΡΠΎΠ³ΡΠ°ΠΌΠΌΡ: Adobe Acrobat.Π’ΡΡΠ΄Ρ ΡΠΎΡΡΡΠ΄Π½ΠΈΠΊΠΎΠ² Π‘ΠΠΠ£(ΡΠ»Π΅ΠΊΡΡΠΎΠ½. Π²Π΅ΡΡΠΈΡ)
System Analysis of Space Missions [ΠΠ»Π΅ΠΊΡΡΠΎΠ½Π½ΡΠΉ ΡΠ΅ΡΡΡΡ] : electronic laboratory course
The present laboratory practice on discipline Β«System Analysis of Space MissionsΒ» urged to give practical skills in carrying out of the complex analysis of almost any typical missions in a circumterraneous space. Problems in a practical work represent a cΠ’ΡΡΠ΄Ρ ΡΠΎΡΡΡΠ΄Π½ΠΈΠΊΠΎΠ² Π‘ΠΠΠ£(ΡΠ»Π΅ΠΊΡΡΠΎΠ½. Π²Π΅ΡΡΠΈΡ).ΠΡΠΏΠΎΠ»ΡΠ·ΡΠ΅ΠΌΡΠ΅ ΠΏΡΠΎΠ³ΡΠ°ΠΌΠΌΡ: Adobe Acrobat
The Repercussion ot Natural and TechnogeniΡ Ore-Gold Objects in Litogeochemical and Biogeochemical Fields
ΠΡΡΠ»Π΅Π΄ΠΎΠ²Π°Π½ΠΈΠ΅ Π²ΡΠΏΠΎΠ»Π½Π΅Π½ΠΎ Π² ΡΠ°ΠΌΠΊΠ°Ρ
Π³Π΅ΠΎΠ»ΠΎΠ³ΠΎ-ΠΏΠΎΠΈΡΠΊΠΎΠ²ΡΡ
ΡΠ°Π±ΠΎΡ Π½Π° ΠΡΠ±ΠΊΠΎΡΡΠΊΠΎΠΉ Π·ΠΎΠ»ΠΎΡΠΎΠ½ΠΎΡΠ½ΠΎΠΉ
ΠΏΠ»ΠΎΡΠ°Π΄ΠΈ, ΠΎΠ³ΡΠ°Π½ΠΈΡΠΈΠ²Π°ΡΡΠ΅ΠΉ ΡΡΠ°Π³ΠΌΠ΅Π½Ρ ΠΎΠ΄Π½ΠΎΠΈΠΌΠ΅Π½Π½ΠΎΠ³ΠΎ Π³ΡΠ°Π±Π΅Π½Π°, Π·Π°ΠΊΠ»ΡΡΠ΅Π½Π½ΠΎΠ³ΠΎ Π² ΡΡΡΡΠΊΡΡΡΠ°Ρ
ΡΠΊΠ»Π°Π΄ΡΠ°ΡΠΎΠ³ΠΎ ΠΎΠ±ΡΠ°ΠΌΠ»Π΅Π½ΠΈΡ ΠΠ½Π³Π°ΡΠΎ-Π’ΡΠ½Π³ΡΡΡΠΊΠΎΠΉ ΠΈ Π’Π°ΡΠ°ΡΡΠΊΠΎΠΉ Π·ΠΎΠ½. Π¦Π΅Π»ΡΡ ΠΈΡΡΠ»Π΅Π΄ΠΎΠ²Π°Π½ΠΈΡ ΡΡΠ°Π»Π° ΠΎΡΠ΅Π½ΠΊΠ°
ΠΏΠΎΠΈΡΠΊΠΎΠ²ΠΎΠΉ ΠΈΠ½ΡΠΎΡΠΌΠ°ΡΠΈΠ²Π½ΠΎΡΡΠΈ Π»ΠΈΡΠΎ- ΠΈ Π±ΠΈΠΎΠ³Π΅ΠΎΡ
ΠΈΠΌΠΈΡΠ΅ΡΠΊΠΈΡ
ΠΌΠ΅ΡΠΎΠ΄ΠΎΠ² ΠΈ ΠΈΠ·ΡΡΠ΅Π½ΠΈΡ Π²ΠΎΠ·ΠΌΠΎΠΆΠ½ΠΎΡΡΠΈ
ΠΈΡΠΏΠΎΠ»ΡΠ·ΠΎΠ²Π°Π½ΠΈΡ ΠΈΡ
Π΄Π»Ρ ΡΠ°Π·Π±ΡΠ°ΠΊΠΎΠ²ΠΊΠΈ ΠΏΡΠΈΡΠΎΠ΄Π½ΡΡ
ΠΈ ΡΠ΅Ρ
Π½ΠΎΠ³Π΅Π½Π½ΡΡ
Π³Π΅ΠΎΡ
ΠΈΠΌΠΈΡΠ΅ΡΠΊΠΈΡ
Π°Π½ΠΎΠΌΠ°Π»ΠΈΠΉ Π·ΠΎΠ»ΠΎΡΠ°This research wass carried ouy within the geological-searching works on the auriferous Dubkosh
area, which bounds the fragment of the same named graben. This graben is confined in the structures
of plicated framing. The estimate of searching informativity of litogeochemical and biogeochemical
methods and studying the possibility of using them for separation natural and tecnogenic geochemical
gold anomalies was the purpose of this researc
The Repercussion ot Natural and TechnogeniΡ Ore-Gold Objects in Litogeochemical and Biogeochemical Fields
ΠΡΡΠ»Π΅Π΄ΠΎΠ²Π°Π½ΠΈΠ΅ Π²ΡΠΏΠΎΠ»Π½Π΅Π½ΠΎ Π² ΡΠ°ΠΌΠΊΠ°Ρ
Π³Π΅ΠΎΠ»ΠΎΠ³ΠΎ-ΠΏΠΎΠΈΡΠΊΠΎΠ²ΡΡ
ΡΠ°Π±ΠΎΡ Π½Π° ΠΡΠ±ΠΊΠΎΡΡΠΊΠΎΠΉ Π·ΠΎΠ»ΠΎΡΠΎΠ½ΠΎΡΠ½ΠΎΠΉ
ΠΏΠ»ΠΎΡΠ°Π΄ΠΈ, ΠΎΠ³ΡΠ°Π½ΠΈΡΠΈΠ²Π°ΡΡΠ΅ΠΉ ΡΡΠ°Π³ΠΌΠ΅Π½Ρ ΠΎΠ΄Π½ΠΎΠΈΠΌΠ΅Π½Π½ΠΎΠ³ΠΎ Π³ΡΠ°Π±Π΅Π½Π°, Π·Π°ΠΊΠ»ΡΡΠ΅Π½Π½ΠΎΠ³ΠΎ Π² ΡΡΡΡΠΊΡΡΡΠ°Ρ
ΡΠΊΠ»Π°Π΄ΡΠ°ΡΠΎΠ³ΠΎ ΠΎΠ±ΡΠ°ΠΌΠ»Π΅Π½ΠΈΡ ΠΠ½Π³Π°ΡΠΎ-Π’ΡΠ½Π³ΡΡΡΠΊΠΎΠΉ ΠΈ Π’Π°ΡΠ°ΡΡΠΊΠΎΠΉ Π·ΠΎΠ½. Π¦Π΅Π»ΡΡ ΠΈΡΡΠ»Π΅Π΄ΠΎΠ²Π°Π½ΠΈΡ ΡΡΠ°Π»Π° ΠΎΡΠ΅Π½ΠΊΠ°
ΠΏΠΎΠΈΡΠΊΠΎΠ²ΠΎΠΉ ΠΈΠ½ΡΠΎΡΠΌΠ°ΡΠΈΠ²Π½ΠΎΡΡΠΈ Π»ΠΈΡΠΎ- ΠΈ Π±ΠΈΠΎΠ³Π΅ΠΎΡ
ΠΈΠΌΠΈΡΠ΅ΡΠΊΠΈΡ
ΠΌΠ΅ΡΠΎΠ΄ΠΎΠ² ΠΈ ΠΈΠ·ΡΡΠ΅Π½ΠΈΡ Π²ΠΎΠ·ΠΌΠΎΠΆΠ½ΠΎΡΡΠΈ
ΠΈΡΠΏΠΎΠ»ΡΠ·ΠΎΠ²Π°Π½ΠΈΡ ΠΈΡ
Π΄Π»Ρ ΡΠ°Π·Π±ΡΠ°ΠΊΠΎΠ²ΠΊΠΈ ΠΏΡΠΈΡΠΎΠ΄Π½ΡΡ
ΠΈ ΡΠ΅Ρ
Π½ΠΎΠ³Π΅Π½Π½ΡΡ
Π³Π΅ΠΎΡ
ΠΈΠΌΠΈΡΠ΅ΡΠΊΠΈΡ
Π°Π½ΠΎΠΌΠ°Π»ΠΈΠΉ Π·ΠΎΠ»ΠΎΡΠ°This research wass carried ouy within the geological-searching works on the auriferous Dubkosh
area, which bounds the fragment of the same named graben. This graben is confined in the structures
of plicated framing. The estimate of searching informativity of litogeochemical and biogeochemical
methods and studying the possibility of using them for separation natural and tecnogenic geochemical
gold anomalies was the purpose of this researc