TY  - RPRT
TI  - Conjugating binary systems for spacecraft thermal control. Appendix C: Aeroassist Flight Experiment Carrier Vehicle preliminary stress analysis
AU  - Ingram, J. E.
AU  - Murray, T. O.
PY  - 1989
UR  - https://ntrs.nasa.gov/citations/19890015890
ID  - 19890015890
ER  -