Fig. 1. Angle of view sketch map

Fig. 2. Temperature and main component mass fraction of exhaust plume at typical time of launching stage

Fig. 3. Exhaust plume IR radiation distribution at typical time of launching stage

Fig. 4. Radiation intensity of component in exhaust plume at typical time of launching stage( H =31.4 km)

Fig. 5. Reentry trajectory and typical trajectory point

Fig. 6. Temperature and component mass fraction distribution of warhead flowfield at reentry stage( H =50 km)

Fig. 7. Temperature and IR radiation contour of warhead at reentry stage(H =50 km)

Fig. 8. Radiation of warhead and flow at typical time of reentry stage