Modeling and validation of Ku-band signal attenuation through rocket plumes

B.J. Veek, van der, S. Chintalapati, D.R. Kirk, H. Gutierrez, R.F. Bun

    Onderzoeksoutput: Bijdrage aan tijdschriftTijdschriftartikelAcademicpeer review

    4 Citaten (Scopus)

    Samenvatting

    Communications to and from a launch vehicle during ascent are of critical importance to the success of rocket-launch operations. During ascent, the rocket's exhaust plume causes significant interference in the radio communications between the vehicle and ground station. This paper presents an improved line of sight: a lower-collision-frequency microwave signal attenuation model based on the plume chemistry, microwave path, and the cross section for momentum transfer. The proposed model considers the combustion products in the exhaust plume, ambient air entrainment downstream of the nozzle, and a plasma attenuation model to estimate the total radio-frequency signal attenuation. The proposed model is benchmarked against measurements of signal attenuation through an exhaust plume in the 12.4 to 18 GHz frequency range.
    Originele taal-2Engels
    Pagina's (van-tot)992-1001
    TijdschriftJournal of Spacecraft and Rockets
    Volume50
    Nummer van het tijdschrift5
    DOI's
    StatusGepubliceerd - 2013

    Vingerafdruk

    Duik in de onderzoeksthema's van 'Modeling and validation of Ku-band signal attenuation through rocket plumes'. Samen vormen ze een unieke vingerafdruk.

    Citeer dit