Heat Shield Cavity Parametric Experimental Aeroheating for a Proposed Mars Smart Lander Aeroshell.

Heat Shield Cavity Parametric Experimental Aeroheating for a Proposed Mars Smart Lander Aeroshell.

Author(s):

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA Fluid Dynamics Conference

Ser. no.:

2002

Pub. Year:

2002

No.:

2002-2746

Paper no.:

2002-2746

Pages:

10

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00001702
Series ID:	PA00000147
Conf. info. (Name):	AIAA Fluid Dynamics Conference and Exhibit
Conf. info. (Number):	32nd
Conf. info. (Venue):	St. Louis, MO
Conf. info. (Date):	2002.06.24-2002.06.26
Note for article:	32nd AIAA Fluid Dynamics Conference and Exhibit, St. Louis, Missouri, 24-26 June 2002

Similar Items:

1 Technical Paper Control Surface and Afterbody Experimental Aeroheating for a Proposed Mars Smart Lander Aeroshell Liechty, D., Edquist, K., Hollis, B. American Institute of Aeronautics and Astronautics	7 Technical Paper Preliminary Aerothermodynamics of Titan Aerocapture Aeroshell Takashima, N., Hollis, B.R., Zoby, E.V., Sutton, K., Olejniczak, J., Prabhu, D. American Institute of Aeronautics and Astronautics
2 Technical Paper Boundary Layer Transition Correlations and Aeroheating Predictions for Mars Smart Lander. Hollis, B.R., Liechty, D.S. American Institute of Aeronautics and Astronautics	8 Technical Paper Heating Augmentation in Laminar Flow Due to Heat-Shield Cavities on the Project Orion CEV B. Hollis American Institute of Aeronautics and Astronautics
3 Technical Paper Aeroheating Environments for a Mars Smart Lander Edquist, K., Liechty, D., Hollis, B., Alter, S., Loomis, M. American Institute of Aeronautics and Astronautics	9 Technical Paper Aeroheating Analysis for the Mars Reconnaissance Orbiter with Comparison to Flight Data D. Liechty American Institute of Aeronautics and Astronautics
4 Technical Paper X-33 experimental aeroheating at Mach 6 using phosphor thermography Horvath, T.J., Berry, S.A., Hollis, B.R., Liechty, D.S., Hamilton, H.H., II, Merski, N.R. American Institute of Aeronautics and Astronautics	10 Technical Paper Heating augmentation due to compression pad cavities on the Project Orion CEV heat shield Hollis, Brian R. American Institute of Aeronautics and Astronautics
5 Technical Paper X-33 Experimental Aeroheating at Mach 6 Using Phosphor Thermography Horvath, T. J., Berry, S. A., Hollis, B. R., Liechty, D. S., Hamilton, H. H., II, Merski, N. R. American Institute of Aeronautics and Astronautics	11 Technical Paper Aerothermodynamic Testing of Protuberances and Penetrations on the NASA Crew Exploration Vehicle Heat Shield D. Liechty American Institute of Aeronautics and Astronautics
6 Technical Paper Comparison of Methods for Determining Boundary Layer Edge Conditions for Transition Correlations Liechty, D.S., Berry, S.A., Hollis, B.R., Horvath, T.J. American Institute of Aeronautics and Astronautics	12 Technical Paper Mars Smart Lander Simulations for Entry, Descent, and Landing Striepe, S., Balaram, B., Way, D., Dwyer, A. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12