Abstract: The present invention relates to a bullet with an increased effective range. The bullet includes a front end portion (10) having a hemispherical shape, a recess portion (20) connected to a rear end of the front end portion (10) and having a curved surface that is recessed inward, an inclined portion (30) connected to a rear end of the recess portion (20) and inclined at a predetermined angle (A) with respect to a horizontal line, a stepped portion (40) connected to a rear end of the inclined portion (30) and inclined at a predetermined angle (A?) with respect to the horizontal line, and fluid inducing grooves formed from the rear to a rear end surface of the bullet (1). Thus, when the bullet passes through underwater, super cavitation may be more effectively generated and maintained for even longer to significantly increase the effective range of the bullet.

Abstract: The present invention relates to a bullet with an increased effective range. The bullet includes a front end portion (10) having a hemispherical shape, a recess portion (20) connected to a rear end of the front end portion (10) and having a curved surface that is recessed inward, an inclined portion (30) connected to a rear end of the recess portion (20) and inclined at a predetermined angle (A) with respect to a horizontal line, a stepped portion (40) connected to a rear end of the inclined portion (30) and inclined at a predetermined angle (A?) with respect to the horizontal line, and fluid inducing grooves formed from the rear to a rear end surface of the bullet (1). Thus, when the bullet passes through underwater, super cavitation may be more effectively generated and maintained for even longer to significantly increase the effective range of the bullet.

Abstract: A method for constructing air-observed terrain data by using a rotary wing structure includes setting flight information including a photographing starting location and a photographing ending location on the basis of a flight route and a photographing location of the rotary wing structure; transmitting, to the rotary wing structure, the flight information so as to store the flight information in a flight control unit; capturing a ground image by a photographing unit of the rotary wing structure and storing the ground image in a storage unit when the rotary wing structure arrives at the photographing location; ending photographing and returning to the ground when the rotary wing structure arrives at the photographing ending location while repeatedly capturing a ground image; and constructing, by a computer in the control center, terrain data by using ground images stored in the storage unit.

Abstract: A method for constructing air-observed terrain data by using a rotary wing structure includes setting flight information including a photographing starting location and a photographing ending location on the basis of a flight route and a photographing location of the rotary wing structure; transmitting, to the rotary wing structure, the flight information so as to store the flight information in a flight control unit; capturing a ground image by a photographing unit of the rotary wing structure and storing the ground image in a storage unit when the rotary wing structure arrives at the photographing location; ending photographing and returning to the ground when the rotary wing structure arrives at the photographing ending location while repeatedly capturing a ground image; and constructing, by a computer in the control center, terrain data by using ground images stored in the storage unit.