WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.30 TO 1.14 OF THE STATIC AERODYNAMIC CHARACTERISTICS OF MODIFIED MERCURY ESCAPE AND EXIT CAPSULE CONFIGURATIONS
Overview & Synopsis
Static aerodynamic characteristics of modified mercury escape and exit capsule configurations at mach numbers 0.30 to 1.4
Indexed from repository: NASA Technical Reports Server
(
ntrs.nasa.gov)
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| Document Title | WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.30 TO 1.14 OF THE STATIC AERODYNAMIC CHARACTERISTICS OF MODIFIED MERCURY ESCAPE AND EXIT CAPSULE CONFIGURATIONS |
|---|---|
| Author / Organization | Pearson, A. D. |
| Subject & Discipline | TECHNICAL_MEMORANDUM |
| Categories | Aerospace & Aviation |
| Publication Year | 2019 |
| License / Rights | Public Domain / NASA STI Open Access |
| Resource Verification | Listed PDF (Verification Pending) |
| Original Host Website |
NASA Technical Reports Server
(ntrs.nasa.gov)
|
| File Format | application/pdf (Portable Document Format) |
| Language | EN |
| Catalog ID | DOC-72823 |
| Original Source Link | Visit Source Page on ntrs.nasa.gov » |