Misunderstanding of dipmeter log in geologic structure interpretation is analysed.

析地层倾角资料构造解释的误区。

According to the characteristics of the electronic instrument of dipmeter, a testing device is developed with computer control technology.

根据倾角电子仪的特点,利用数控测试技术,研制开发了倾角电子仪的测试装置。

By the analysis, it has been concluded that slopy ridge has better discharge effect comparing with verical ridge.

结论-试验证明，斜墙式力坎的倾角越大，能率越大，同时收缩端面处的回漩流速也更大。

Determining the attainability domain of aeroassisted orbital plane change, i.e. the inclination and the longitude of the ascending node, is a very important problem.

航天器进行气动力辅助异面变轨时，确定可达范围(变轨结束时的倾角和升交点赤经)是一个十重要的问题。

Misunderstanding of dipmeter log in geologic structure interpretation is analysed.

分析地层倾资料构造解释的误区。

According to the characteristics of the electronic instrument of dipmeter, a testing device is developed with computer control technology.

根据倾电子仪的特点,利用数控测试技术,研制开发了倾电子仪的测试装置。

By the analysis, it has been concluded that slopy ridge has better discharge effect comparing with verical ridge.

结论-试验证明，斜墙式力坎的倾，，同时收缩端面处的回漩流速也更。

Determining the attainability domain of aeroassisted orbital plane change, i.e. the inclination and the longitude of the ascending node, is a very important problem.

航天器进行气动力辅助异面变轨时，确定可达范围(变轨结束时的倾和升交点赤经)是一个十分重要的问题。

Misunderstanding of dipmeter log in geologic structure interpretation is analysed.

分析地层倾角资料构造解释的误区。

According to the characteristics of the electronic instrument of dipmeter, a testing device is developed with computer control technology.

根据倾角电子仪的特点,利用试技术,研制开发了倾角电子仪的试装置。

By the analysis, it has been concluded that slopy ridge has better discharge effect comparing with verical ridge.

结论-试验证明，斜墙式力坎的倾角越大，能率越大，同时收缩端面处的回漩流速也更大。

Determining the attainability domain of aeroassisted orbital plane change, i.e. the inclination and the longitude of the ascending node, is a very important problem.

航天器进行气动力辅助异面变轨时，确范围(变轨结束时的倾角和升交点赤经)是一个十分重要的问题。

Misunderstanding of dipmeter log in geologic structure interpretation is analysed.

分析地层倾角资料构造解释的误区。

According to the characteristics of the electronic instrument of dipmeter, a testing device is developed with computer control technology.

根据倾角电子仪的特点,利用数控测试技术,研制开发了倾角电子仪的测试装置。

By the analysis, it has been concluded that slopy ridge has better discharge effect comparing with verical ridge.

结论-试验证明，斜墙式力坎的倾角越大，能率越大，同时收缩端面处的回漩流速也更大。

Determining the attainability domain of aeroassisted orbital plane change, i.e. the inclination and the longitude of the ascending node, is a very important problem.

航天器进行气动力辅助异面变轨时，确定可达范围(变轨结束时的倾角和升交点赤经)是一个十分重要的问题。

Misunderstanding of dipmeter log in geologic structure interpretation is analysed.

分析地层倾角资料构造误区。

According to the characteristics of the electronic instrument of dipmeter, a testing device is developed with computer control technology.

根据倾角电子仪特点,利用数控测试技术,研制开发了倾角电子仪测试装置。

By the analysis, it has been concluded that slopy ridge has better discharge effect comparing with verical ridge.

结论-试验证明，斜墙式力坎倾角越大，能率越大，同时收缩端面处回漩流速也更大。

Determining the attainability domain of aeroassisted orbital plane change, i.e. the inclination and the longitude of the ascending node, is a very important problem.

航天器进行气动力辅助异面变轨时，确定可达范围(变轨结束时倾角和升交点)一个十分重要问题。

Misunderstanding of dipmeter log in geologic structure interpretation is analysed.

分析地层倾角资料构造解释误区。

According to the characteristics of the electronic instrument of dipmeter, a testing device is developed with computer control technology.

根据倾角电特点,利用数控测试技术,研制开发了倾角电测试装置。

By the analysis, it has been concluded that slopy ridge has better discharge effect comparing with verical ridge.

论-试验证明，斜墙式力坎倾角越大，能率越大，同收缩端面处回漩流速也更大。

Determining the attainability domain of aeroassisted orbital plane change, i.e. the inclination and the longitude of the ascending node, is a very important problem.

航天器进行气动力辅助异面变轨，确定可达范围(变轨倾角和升交点赤经)是一个十分重要问题。

Misunderstanding of dipmeter log in geologic structure interpretation is analysed.

分析地层倾角资料构造解释误区。

According to the characteristics of the electronic instrument of dipmeter, a testing device is developed with computer control technology.

根据倾角特点,利用数控测试技术,研制开发了倾角测试装置。

By the analysis, it has been concluded that slopy ridge has better discharge effect comparing with verical ridge.

结论-试验证明，斜墙式力坎倾角越大，能率越大，同收缩端面处回漩流速也更大。

Determining the attainability domain of aeroassisted orbital plane change, i.e. the inclination and the longitude of the ascending node, is a very important problem.

航天器进行气动力辅助异面变轨，确定可达范围(变轨结倾角和升交点赤经)是一个十分重要问题。

Misunderstanding of dipmeter log in geologic structure interpretation is analysed.

分析地层倾角资料构造解释的误区。

According to the characteristics of the electronic instrument of dipmeter, a testing device is developed with computer control technology.

根据倾角电子仪的特点,利用数控测试技术,研制开发了倾角电子仪的测试装置。

By the analysis, it has been concluded that slopy ridge has better discharge effect comparing with verical ridge.

结论-试验证，斜墙式力坎的倾角越大，能率越大，同时收缩端面处的回漩流速也更大。

Determining the attainability domain of aeroassisted orbital plane change, i.e. the inclination and the longitude of the ascending node, is a very important problem.

航天器进行气动力辅助异面变轨时，确定可达范围(变轨结束时的倾角和升交点赤经)是一个十分重要的问题。

Misunderstanding of dipmeter log in geologic structure interpretation is analysed.

分析地层倾角资料构造解释的误区。

According to the characteristics of the electronic instrument of dipmeter, a testing device is developed with computer control technology.

根据倾角电子仪的特点,控测试技术,研制开发了倾角电子仪的测试装置。

By the analysis, it has been concluded that slopy ridge has better discharge effect comparing with verical ridge.

结论-试验证明，斜墙式力坎的倾角越大，能率越大，同时收缩端面处的回漩流速也更大。

Determining the attainability domain of aeroassisted orbital plane change, i.e. the inclination and the longitude of the ascending node, is a very important problem.

航天器进行气动力辅助异面变轨时，确定可(变轨结束时的倾角和升交点赤经)是一个十分重要的问题。