In-flight motor torque estimates for the second-stage Strypi IX launch vehicle
Conference
·
OSTI ID:7075697
This paper documents the results of a study to determine the character of body fixed torques generated by the Anteres IIA motor, during second-stage burn of the Strypi IX launch vehicle. The Strypi IX is a two-stage spin-stabilized solid-propellant launch vehicle designed to boost a variety of payloads to reentry environment conditions. The torque estimates were determined from postflight analysis of Euler angle telemetry data. Principal axis misalignments, and thrust misalignments were also estimated. Data was analyzed from two separate launches; a Precursor and a Prime flight. 21 figs.
- Research Organization:
- Sandia National Labs., Albuquerque, NM (USA)
- DOE Contract Number:
- AC04-76DP00789
- OSTI ID:
- 7075697
- Report Number(s):
- SAND-87-2755C; CONF-880764-1; ON: DE88010833
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
42 ENGINEERING
420200* -- Engineering-- Facilities
Equipment
& Techniques
657002 -- Theoretical & Mathematical Physics-- Classical & Quantum Mechanics
71 CLASSICAL AND QUANTUM MECHANICS
GENERAL PHYSICS
COMMUNICATIONS
DATA TRANSMISSION
DIFFERENTIAL EQUATIONS
DYNAMICS
ENGINES
EQUATIONS
EQUATIONS OF MOTION
INERTIAL GUIDANCE
LAUNCHING
MATHEMATICAL MODELS
MECHANICS
PARTIAL DIFFERENTIAL EQUATIONS
REENTRY
REENTRY VEHICLES
ROCKET ENGINES
SPACE VEHICLES
TELEMETRY
TORQUE
VEHICLES
420200* -- Engineering-- Facilities
Equipment
& Techniques
657002 -- Theoretical & Mathematical Physics-- Classical & Quantum Mechanics
71 CLASSICAL AND QUANTUM MECHANICS
GENERAL PHYSICS
COMMUNICATIONS
DATA TRANSMISSION
DIFFERENTIAL EQUATIONS
DYNAMICS
ENGINES
EQUATIONS
EQUATIONS OF MOTION
INERTIAL GUIDANCE
LAUNCHING
MATHEMATICAL MODELS
MECHANICS
PARTIAL DIFFERENTIAL EQUATIONS
REENTRY
REENTRY VEHICLES
ROCKET ENGINES
SPACE VEHICLES
TELEMETRY
TORQUE
VEHICLES