Abstract: The safe operation of pyrolytic-based, hazardous waste processing systems is accomplished by rapidly controlling an oxygen to product gas ratio and pressures within such systems.
Type:
Grant
Filed:
September 22, 2000
Date of Patent:
April 22, 2003
Assignee:
Vanguard Research, Inc.
Inventors:
Yuji Kado, John F. Kantak, Jay Ramamurthi, Mark E. Vetter
Abstract: A space vehicle has two stages: one containing an air motor; the other containing a rocket propellent motor. After the space vehicle has been launched, flexible wings such as parafoils can be used to recover stages of the space vehicle. In addition, flexible wings such as a parafoil can be used to aid in the delivery payload in the second stage into its orbital state.