File:High-energy Photon bus releases the entry probe 30 min before entry interface (EI) after targeting the entry interface selected for optimal instrument measurement conditions (Rocket Lab Mission to Venus).webp

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Captions

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From the paper "Rocket Lab Mission to Venus"

Summary

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Description
English: "In October 2023, after the cruise phase (Figure 5), high energy Photon will target an entry interface to deploy a small (~20 kg) probe directly into the atmosphere with an entry flight path angle (EFPA) between −10 and −30 degrees, with a baseline of −10 degrees. The probe communicates direct-to-Earth through an S-band communications link with a hemispherical antenna returning science data captured during the descent and stored on board. The entry interface will be selected to satisfy science objectives (night-side entry and latitude targeting), Earth communication geometry, and other factors. The EFPA will be selected based on an analysis of the entry and descent timeline, the integrated heat load and required thermal protection system (TPS) thickness, probe acceleration (g-loading) limits, navigation precision, and other factors."
Date
Source https://www.mdpi.com/2226-4310/9/8/445/htm
Author

Authors of the study:

Richard French, Christophe Mandy, Richard Hunter, Ehson Mosleh, Doug Sinclair, Peter Beck, Sara Seager, Janusz J. Petkowski, Christopher E. Carr, David H. Grinspoon, Darrel Baumgardner, and on behalf of the Rocket Lab Venus Team

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w:en:Creative Commons
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current10:52, 22 September 2022Thumbnail for version as of 10:52, 22 September 20223,662 × 1,866 (1.19 MB)Prototyperspective (talk | contribs)Uploaded a work by Authors of the study: Richard French, Christophe Mandy, Richard Hunter, Ehson Mosleh, Doug Sinclair, Peter Beck, Sara Seager, Janusz J. Petkowski, Christopher E. Carr, David H. Grinspoon, Darrel Baumgardner, and on behalf of the Rocket Lab Venus Team from https://www.mdpi.com/2226-4310/9/8/445/htm with UploadWizard

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