Mars Phoenix Entry, Descent, and Landing Trajestory and Atmosphere Reconstruction-Reference-Cited by-同舟云学术

Mars Phoenix Entry, Descent, and Landing Trajestory and Atmosphere Reconstruction

Published:2011-09 Issue:5 Volume:48 Page:809-822
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Blanchard Robert C.¹,Desai Prasun N.²

Affiliation:

1. George Washington University, Hampton, Virginia 23681-2199

2. NASA Langley Research Center, Hampton, Virginia 23681-2199

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.46274

Reference12 articles.

1. Introduction to special section on the Phoenix Mission: Landing Site Characterization Experiments, Mission Overviews, and Expected Science

2. Entry, Descent, and Landing Performance of the Mars Phoenix Lander

3. Overview of the Phoenix Entry, Descent, and Landing System Architecture

4. Measurements of thermal structure and thermal contrasts in the atmosphere of Venus and related dynamical observations: Results From the four Pioneer Venus Probes

5. Compton, H. R., Blanchard, R. C., and Findlay, J. T. "Shuttle Entry Trajectory Reconstruction Using In-Flight Accelerometer and Gyro Measurements," AIAA Paper 79-0257, Jan. 1079.

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