RU2016150068A3 - - Google Patents
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- RU2016150068A3 RU2016150068A3 RU2016150068A RU2016150068A RU2016150068A3 RU 2016150068 A3 RU2016150068 A3 RU 2016150068A3 RU 2016150068 A RU2016150068 A RU 2016150068A RU 2016150068 A RU2016150068 A RU 2016150068A RU 2016150068 A3 RU2016150068 A3 RU 2016150068A3
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Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2016150068A RU2662371C2 (en) | 2016-12-19 | 2016-12-19 | Method for determining atmospheric density at spacecraft height of flight |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2016150068A RU2662371C2 (en) | 2016-12-19 | 2016-12-19 | Method for determining atmospheric density at spacecraft height of flight |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| RU2016150068A RU2016150068A (en) | 2018-06-20 |
| RU2016150068A3 true RU2016150068A3 (en) | 2018-06-20 |
| RU2662371C2 RU2662371C2 (en) | 2018-07-25 |
Family
ID=62619398
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2016150068A RU2662371C2 (en) | 2016-12-19 | 2016-12-19 | Method for determining atmospheric density at spacecraft height of flight |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2662371C2 (en) |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6454215B1 (en) * | 2001-01-29 | 2002-09-24 | Lockheed Martin Corporation | Spacecraft architecture for disturbance-free payload |
| RU2463223C1 (en) * | 2011-03-30 | 2012-10-10 | Открытое акционерное общество "Российская корпорация ракетно-космического приборостроения и информационных систем" (ОАО "Российские космические системы") | Method of determination and prediction of subjected to atmospheric braking aircraft motion on low orbits |
| CN104090493B (en) * | 2014-05-27 | 2016-05-11 | 北京航空航天大学 | A kind of inclined to one side interference compensation control method without towing satellite based on accelerometer |
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2016
- 2016-12-19 RU RU2016150068A patent/RU2662371C2/en active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2016150068A (en) | 2018-06-20 |
| RU2662371C2 (en) | 2018-07-25 |