Aerodynamic Stability and Control, Data, Model 844-2035

reportActive / Technical Report | Accession Number: AD0756854 | Open PDF

Abstract:

The aerodynamic stability and control characteristics of the 844-2035 Dyna Soar glider are presented. These data are based on wind tunnel tests, where data are available. Where not available, theoretical estimates have been made for the vehicle characteristics. This is the interim glider configurations. Some vehicle characteristics peculiar to this configuration are not satisfactory and will be modified for the final configuration. The data presented will be revised as additional wind tunnel data are received and better estimates of the vehicle characteristics are made.

Author(s):
No Author(s) Identified
Author Organization(s):
BOEING CO SEATTLE WA
Supplementary Note:
Availability: Available in microfiche only.
Pagination:
0197

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release, Document Partially Illegible
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited. Document Partially Illegible.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
D2-8174
Contract/Grant Number(s):
AF 33(600)-41517
Monitor Series:
USAF
 Subject Terms
Joint Capability Areas:
JCA_1.1_Force Management; JCA_1_Force Support; JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means; JCA_6_Net Centric
Communities of Interest:
Air Platforms
Descriptor(s):
*LIFTING REENTRY VEHICLES, *RENDEZVOUS SPACECRAFT, STABILITY, AERODYNAMIC CHARACTERISTICS, AEROSPACE CRAFT, BRAKING, AERODYNAMIC CONTROL SURFACES, LANDING, HYPERSONIC FLIGHT, SUPERSONIC FLIGHT, TRANSONIC FLIGHT
Field(s)/Group(s):
Fluid Mechanics, Unmanned Spacecraft
Keyword(s):
X 20 SPACECRAFT, SPACE SHUTTLES, SPACECRAFT MODIFICATION
Report Date:
1972 Feb 14