SP-4012 NASA HISTORICAL DATA BOOK: VOLUME III
PROGRAMS AND PROJECTS 1969-1978

 

Table 3-102. ISIS 1 Characteristics

 

Also called:

International Satellite for Ionospheric Studies

Memorandum of Understanding (MOU)

between NASA and the Canadian Defense Research Board and the Canadian Dept. of Communications, 1963

Date of launch (range):

Jan 30, 1969 (WTR)

Launch vehicle:

Delta Standard Vehicle 3E

Shape:

oblate spheroid (8-sided)

Weight (kg):

236

Dimensions (m):

1.27, diam.

1.07, height

Power source:

solar cells plus 3 NiCd batteries

Prime contractor:

CA Victor Co., Montreal

Date of reentry:

N/A

NASA's role:

launch vehicle, technical support, tracking and data acquisition; participation in experimental program

Responsible NASA center:

GSFC

Project manager:

Evart D. Nelson

Project scientist:

John E. Jackson

Objectives:

To continue to extend a joint U.S.-Canadian program of ionospheric studies by combining sounder data with correlative direct measurements for a time sufficient to cover latitudinal and diurnal variations during a period of high solar activity.

Experiments (responsible country or organization):

.

swept frequency sounder (Defense Research Telecommunications Establishment)

fixed frequency sounder (DRTE)

VLF receiver/exciter (DRTE)

radio beacon (Univ. of Western Ontario)

cosmic radio noise (DRTE)

energetic particle detector (National Research Council, Canada)

ion mass spectrometer (Air Force Cambridge Research Laboratories, U.S.)

cylindrical electrostatic probe (GSFC)

spherical electrostatic analyzer (AFCRL)

Results:

Successful; ISIS 1 gave experimenters an opportunity to combine on one satellite direct and indirect measurements of important ionospheric parameters. Data were obtained until Oct. 1979; ISIS 1 was the third in a series of 5 joint experiments with Canada.

Reference: MOR S-850-69-02, Jan. 27, 1969.


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