NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The Malemute development programThe Malemute vehicle systems are two-stage systems based on utilizing a new high performance upper stage motor with two existing military boosters. The Malmute development program is described relative to program structure, preliminary design, vehicle subsystems, and the Malemute motor. Two vehicle systems, the Nike-Malemute and Terrier-Malemute, were developed which are capable of transporting comparatively large diameter (16 in.) 200-lb payloads to altitudes of 500 and 700 km, respectively. These vehicles provide relatively low-cost transportation with two-stage reliability and launch simplicity. Flight tests of both vehicle systems revealed their performance capabilities, with the Terrier-Malemute system involving a unique Malemute motor spin sensitivity problem. It is suggested that the vehicles can be successfully flown by lowering the burnout spin rate.
Document ID
19760052771
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bolster, W. J.
(NASA Goddard Space Flight Center Greenbelt, Md., United States)
Hoekstra, P. W.
(Thiokol Corp. Ogden, Utah, United States)
Date Acquired
August 8, 2013
Publication Date
June 1, 1976
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AIAA PAPER 76-1867
Meeting Information
Meeting: Sounding Rocket Technology Conference
Location: Boston, MA
Start Date: June 23, 1976
End Date: June 25, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A35737
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available