Beberapa Tjatatan Mengenai Roket

K. Purbosiswojo

Abstract


Ichtisar. Dalam karangan ini didjelaskan beberapa persamaan untuk roket ideal. Dalam roket ideal ini termasuk roket jang pengurangan bahan bakarnja tiap waktu adalah konstan dan roket jang gaja dorongnja konstan dalam segala keadaan tekanan udarannja statis dan ketinggian roket dari permukaan air laut.

 

Abstract. In this paper some equations for idealized rockets are discussed. This type of rockets include those which rate of mass-change is constant and those which thrust is constant in any kind of condition of static pressure and altitude.


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References


Miele, A., 1962, Flight – Mechanics I, Addison Wesley Publ. Co.

v.d. Kamp, P., 1962, JRAS of Canada 56, 157.

Summerfield, M. and Seifert, H.S., 1959, Space Technology, Chapter 3, John Wiley and Sons, Inc.

Nelson, W.C. and Loft, E.E., Space Mechanics, 1962, Prentice Hall, Inc.


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