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040 |aCaOODSP|beng|erda|cCaOODSP
043 |an-cn---
0861 |aCo24-203/1975E-PDF
24500|aUHF/SHF/L-band spacecraft trade offs & budgets : |bfinal report / |cRCA Limited.
264 1|aOttawa, Ontario : |bDepartment of Communications, |cApril 1975.
300 |a1 online resource (v, 64 pages) : |bfigures
336 |atext|btxt|2rdacontent
337 |acomputer|bc|2rdamedia
338 |aonline resource|bcr|2rdacarrier
500 |aDigitized edition from print [produced by Innovation, Science and Economic Development Canada].
520 |a"Two transponder configurations were investigated. The first was a single band UHF spacecraft with the proviso that the complete UHF band be translated to 7 GHz for transmission to the ground where all signal processing was to take place. All signals were then assembled at 80Hz for transmission to the spacecraft. The signal band is then translated back to the UHF band for broadcast to the mobile field units. The UHF transponder was sized to fully occupy the payload of a 3-axis stabalized spacecraft suitable for launch on a 3914 Thor Delta vehicle"--Foreword.
69207|2gccst|aTelecommunications
69207|2gccst|aSpace technology
7101 |aCanada. |bDepartment of Communications.
7102 |aRCA Limited.
85640|qPDF|s2.85 MB|uhttps://publications.gc.ca/collections/collection_2019/isde-ised/Co24/Co24-203-1975-eng.pdf