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,利用数技术,研制开发了倾角电子仪的装置。

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

结论-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，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.

根据电子仪特点,利用数控测试技术,研制开发了电子仪测试装置。

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，能率，时收缩端面处回漩流速也更。

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.

根据子仪特点,利用数控测试技术,研制开发了子仪测试装置。

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.

析地层倾构造解释的误区。

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(变轨结束时的倾和升交点赤经)是一个要的问题。

Misunderstanding of dipmeter log in geologic structure interpretation is analysed.

分析地层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.

根据子仪的特点,利用数控测试技术,研制开发了子仪的测试装置。

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

结论-试验证明，斜墙式坎的越大，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.

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

Misunderstanding of dipmeter log in geologic structure interpretation is analysed.

析地层倾角造解释的误区。

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。

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

据倾角电子仪的特,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。