Major Documents | |||
Cover | Document | Source | Description |
Hypersonics Before the
Shuttle NASA SP2000-4518 |
pdf on NASA History Division web site |
132-page
NASA monograph by
Dennis R. Jenkins: Monographs in Aerospace
History
Number 18, 2000 |
|
X-15
Research Results NASA SP-60 |
pdf in NTRS archive | 128-page NASA report by Wendell H. Stillwell, 1965 | |
Proceedings
of the X-15 First Flight 30th Anniversary Celebration NASA CP-3105 |
pdf in NASA Dryden Technical Reports Server | 175-page
proceedings of
conference at NASA Dryden commemorating the X-15 research program, June
8, 1989. (File is 26 megabytes) |
|
X-15
Flight Manual North American Aviation T.O. 1X-15-1 (FHB 23-1) |
Scanned from original document | 126-page
manual describing
the X-15 aircraft, its systems, and operating procedures (File is 60 megabytes, this is a high resolution color scan) |
|
Trouble downloading the Flight Manual as 1 huge file? Click here for an index to separate files for each section | |||
X-15 design proposal North American Aviation document 55WCS-9229-AA |
Scanned from photocopy of original document | 62-page design proposal submitted by North American Aviation May 9, 1955 (File is 24 megabytes) |
Technical Reports | |||
Cover | Document | Source | Description |
Flight
Flutter Results
for Flat Rectangular Panels NASA TN D-1058 |
pdf in NTRS archive | 12-page NASA technical note by Eldon E. Kordis and Richard B. Noll, 1962. Studies supersonic flutter of skin panels, comparing theory with flight test results. Describes structural engineering used in X-15 vertical stabilizers and fuselage side fairings to (1) prevent flutter; (2) conserve structural weight; and (3) accomodate thermal stress at hypersonic speeds. | |
Design
Report - Thermal
Protection System X-15A-2 NASA CR-82003 |
pdf in NTRS archive | 322-page
contractor
report to NASA
by A.B. Price, Martin Marietta Corporation, 1968. Describes
the
ablative
material
and related changes designed for flight to Mach 7.4 with X-15A-2. (File is 90 megabytes) |
|
Flight
Experience with
Shock Impingement and Interface Heating on the X-15-2 Research Airplane NASA TM X-1669 |
pdf in NTRS archive | 29-page
NASA
technical memorandum by Joe D. Watts, 1968 Describes and analyzes unpredicted heating on the Mach 6.7 flight of X-15 #2, which produced major unexpected heating damage |