Full-Scale Aerodynamic and Engine Testing of the APL Symdel Mk VI RPV.

Abstract

This report presents documentation of the wind tunnel testing of the APL Symdel Mk VI remotely piloted vehicle (RPV). The purpose of these tests was to determine the aerodynamic features, live engine performance, and active control servo responses of the RPV. Standard six component aerodynamic data are given for six alternative configurations.

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1974
Accession Number
ADA006283

Entities

People

  • M. L. Hill
  • R. H. Cramer

Organizations

  • Johns Hopkins University Applied Physics Laboratory

Tags

Communities of Interest

  • Autonomy

DTIC Thesaurus Topics

  • Remotely Piloted Vehicles
  • Standards
  • Vehicles
  • Wind Tunnels

Readers

  • Aerospace Engineering
  • Aerospace Test and Evaluation