Journal of Astronomy and Space Sciences 제1권 1호

1984.09 서비스 종료(열람 제한)

Journal of Astronomy and Space Sciences 제1권 1호 pp.5-21 한국우주과학회

The airflow along the surface of a launch vehicle together with base flow of clustered nozzles cause problems which may affect the stability or efficiency of the entire vehicle. The problem may occur when the vehicle is on the launching pad or even during flight. As for such problems, local steady-steady-state loads, overall steady-state loads, buffet, ground wind loads, base heating and rocket-nozzle hinge moments are examined here specifically.

1984.09 서비스 종료(열람 제한)

Spacecraft Spin Rate Change due to Propellant Redistribution Between Tanks

Choi, Kyu-Hong

Journal of Astronomy and Space Sciences 제1권 1호 pp.23-34 한국우주과학회

1984.09 서비스 종료(열람 제한)

Space shuttle의 Thermal Protection System의 설계 목표

Design Golas for the Space Shuttle's Thermal Protection System

김선규

Journal of Astronomy and Space Sciences 제1권 1호 pp.35-39 한국우주과학회

1984.09 서비스 종료(열람 제한)

Photoelectric Observations of the Close Eclipsing Binary System CW Cephei

Han, Won-Yong