Flight Mechanics Feasibility Assessment for Co-Delivery of Direct-Entry Probe and Aerocapture Orbiter-Reference-Cited by-同舟云学术

Flight Mechanics Feasibility Assessment for Co-Delivery of Direct-Entry Probe and Aerocapture Orbiter

Published:2022-01 Issue:1 Volume:59 Page:19-32
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Albert Samuel W.¹^ORCID,Schaub Hanspeter¹^ORCID,Braun Robert D.²

Affiliation:

1. University of Colorado Boulder, Boulder, Colorado 80303

2. California Institute of Technology, Pasadena, California 91125

Funder

National Aeronautics and Space Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A34953

Reference40 articles.

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2. CubeSat evolution: Analyzing CubeSat capabilities for conducting science missions

3. NortonC. D.PellegrinoS.JohnsonM. “Small Satellites: A Revolution in Space Science,” Keck Inst. for Space Studies, California Inst. of Technology, Pasadena, CA, July 2014.

4. AsmarS. W.MatousekS., Mars Cube One (MarCO): Shifting the Paradigm in Relay Deep Space Operation, AIAA, Reston, VA, 2016, pp. 1–7.

5. Drag-Modulation Flight-Control System Options for Planetary Aerocapture

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